US4085619A - Electronic balancer for vehicle wheels - Google Patents

Electronic balancer for vehicle wheels Download PDF

Info

Publication number
US4085619A
US4085619A US05/656,606 US65660676A US4085619A US 4085619 A US4085619 A US 4085619A US 65660676 A US65660676 A US 65660676A US 4085619 A US4085619 A US 4085619A
Authority
US
United States
Prior art keywords
signal
wheel
shaft
tire
amplifier
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US05/656,606
Inventor
Haskell Shapiro
Robert E. DeCaro
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BRANICK INDUSTRIES Inc 2600 - 3RD AVE NO FARGO ND A CORP OF ND
Royal Industries Inc
Original Assignee
Royal Industries Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Royal Industries Inc filed Critical Royal Industries Inc
Priority to US05/656,606 priority Critical patent/US4085619A/en
Priority to CA270,478A priority patent/CA1101523A/en
Priority to NL7701065A priority patent/NL7701065A/en
Priority to BE174642A priority patent/BE851064A/en
Priority to DE19772705023 priority patent/DE2705023A1/en
Priority to FR7703574A priority patent/FR2340545A1/en
Priority to IT20077/77A priority patent/IT1085915B/en
Priority to JP1349877A priority patent/JPS5296589A/en
Application granted granted Critical
Publication of US4085619A publication Critical patent/US4085619A/en
Assigned to BRANICK INDUSTRIES, INC., 2600 - 3RD AVE. NO., FARGO, ND A CORP OF ND reassignment BRANICK INDUSTRIES, INC., 2600 - 3RD AVE. NO., FARGO, ND A CORP OF ND ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: RUGBY INDUSTRIES, INC. A CORP. OF ND
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M1/00—Testing static or dynamic balance of machines or structures
    • G01M1/14—Determining imbalance
    • G01M1/16—Determining imbalance by oscillating or rotating the body to be tested
    • G01M1/22—Determining imbalance by oscillating or rotating the body to be tested and converting vibrations due to imbalance into electric variables
    • G01M1/225—Determining imbalance by oscillating or rotating the body to be tested and converting vibrations due to imbalance into electric variables for vehicle wheels

Definitions

  • the prior art with which this invention is concerned contains numerous examples of apparatus and concepts for balancing the wheel-tire systems of a vehicle so as to eliminate destructive and annoying vibrations present at various resonant frequencies of operation caused by static and dynamic imbalances in a wheel-tire system for each of the wheels of a vehicle.
  • the present invention facilitates that balancing of a wheel-tire system by providing an operation whereby the wheel-tire system is mounted upon a shaft that is in turn driven by a motor that is under the control of a system which accepts signals generated by the shaft and its mountings whereby a wheel-tire system is disposed on the shaft and a motor is energized to impart rotation to the shaft and wheel-tire system.
  • Predetermined frequency or angular velocity of the shaft is selected in accordance with the intended operational characteristics of the vehicle upon which the wheel-tire systems are to be used.
  • Sources of signal corresponding to the rotational velocity or speed of the shaft and the angular position of the shaft, resolved to a predetermined angular degree, are utilized to first detect the coincidence of actual speed with predetermined speed for the shaft at which time both of the signals corresponding to speed and angular position are utilized to process the information derived from two or more sources of signal that are responsive to the velocity of displacement of the shaft in a plane.
  • the processing of the information contained in the signals continues for a short predetermined time after which, the motor is energized in such a manner to cause reverse operation and this form of dynamic braking of the motor, which takes place over a very short period of time, brings the wheel-tire system to a rapid stop position, such position being related to the reverse direction of the shaft for a predetermined, short angular motion.
  • the magnitudes of the weights relating to the imbalance of the wheel-tire system may conveniently be displayed on meters calibrated in ounces or grams or other suitable systems of weight measure.
  • further signal responsive means which will energize an indicator such as a lamp, whereby when the wheel-tire system is rotated on the shaft, an angular position for each of the magnitudes of corrective weights will be indicated by illumination of the lamp or other indicator, the angular position being related to the magnitudes and each being related to one of the planes of the wheel that is adjacent the rims, such planes lying in perpendicular disposition with respect to the axis of rotation of the shaft upon which the wheel-tire system is mounted.
  • an indicator such as a lamp
  • FIG. 1 is a schematic and diagrammatic representation of an operational system embodying the principles of our invention
  • FIG. 2 is a side elevational view, partly in section, of a portion of the right end of FIG. 1 showing the relationship between a bearing and a wheel mounted on the shaft;
  • FIGS. 3, 4 and 5 are detailed views showing the relationship of the elements disposed on the left end of FIG. 1 of the drawings.
  • FIGS. 6-6G comprise an electrical schematic diagram incorporating the principles of my invention into a signal processing and motor control system as embodied on FIG. 1 of the drawings, specifically, FIG. 6 illustrates the manner in which FIGS. 6A-6G may be assembled to form a complete electrical and diagrammatic showing of our invention.
  • FIG. 1 of the drawings a diagrammatic representation of a complete balancing machine is indicated generally by reference character 10.
  • the apparatus includes a rotatable shaft 12 having an axis of rotation 12A.
  • a pulley 17 is nonrotatably disposed on shaft 12 and is driven by motor 11 having an output pulley 18 through drive belt 19.
  • Shaft 12 is rotatably journaled in bearings 13 and 14, such bearing being mounted upon a suitable base whereby forces that may be exerted thereon due to an imbalance in a wheel-tire system 20-23, are constrained and do in fact occur substantially within a plane, as indicated by reference character 16.
  • the velocity of the back and forth movement of bearings 13 and 14 within plane 16 may be sensed by suitable velocity detecting transducers 25 and 26 which serve to convert any displacement of bearings 13 and 14, along the directions indicated adjacent them into electrical signals that are representative of such velocity of displacement.
  • a wheel-tire assembly is shown disposed on the right end of shaft 12 by suitable screw threaded means that may be attached to the mounting holes on wheel 20, such mounting is indicated by reference character 24, and as will be discussed below, mounting member 24 is adjustable longitudinally of shaft 12 to provide positioning of one of the planes of rotation of wheel-tire system 20-23 in the plane of rotation of one of the effective portions of one of the bearing members.
  • a position and speed signal generator indicated by reference character 27, includes a plurality of apertures 28 disposed on a common radius and at intervals sufficiently small to provide the required angular resolution of a shaft position during the balancing operations.
  • a further single aperture 29 is shown disposed on a different radius and, as will be explained in more detail below, serves to provide a signal proportional to the rotational velocity of shaft 12.
  • Suitable sources of light disposed in predetermined relationship with apertures 28 and 29 in signal generating member 27, are provided to illuminate a plurality of light sensitive sources of signal indicated by reference characters 31, 32, and 33. Each of these is shown connected through suitable conductors 40, 41, and 42, respectively, to a signal processor and motor control, block.
  • motor 11 is connected to the same block through conductor 45 as are the outputs of velocity of displacement sensors 25 and 26 through conductors 43 and 44, respectively.
  • a pair of indicating lamps 36 and 37, further identified by ⁇ I and ⁇ O, and a pair of indicating meters 34 and 35 are likewise indicated by WO and WI.
  • a wheel-tire system is suitably disposed on mounting clamp 24 and the assembly is locked in place with the plane of rotation of the inner rim of wheel 20 in the plane of rotation of the effective bearing portion of bearing 14 (as seen on the left end of portion 15 of bearing 14).
  • Signal processor and motor control may be operable to initiate operation of the system of energizing motor 11 to drive shaft 12 in a predetermined direction.
  • signal processor and motor control block becomes operative to accept the velocity of displacement signals from sensors 25 and 26 and the velocity and position of rotation as determined through the use of sensors 31, 32 and 33, to make a rapid determination of the amount of weight that is necessary to correct the imbalance of the wheel-tire system and the angular positions that the weights should be added to the wheel-tire system, after which motor 11 is de-energized and then re-energized in a reverse direction to rapidly effect a dynamic breaking of shaft 12 and, upon detection of the reverse revolution of shaft 12 over the predetermined degrees of angular resolution, it would de-energize motor 11 and allow the shaft to remain at rest.
  • meters 35 and 34 indicate the amount of weight to be added to the wheel and tire systems on the inner plane 22 and outer plane 21.
  • Indicators 37 and 36 are energized at this time.
  • the operator manually rotates the wheel-tire system and at the position that the weight is required as indicated on meters 35 and 34, one or the other of indicators 37 and 36 will be energized to indicate to the operator that the correct angular position for adding the weight has been reached.
  • a vertical axis through generally horizontal plane 16 as a reference so that the operator will know where to attach the indicated corrective weight to each of the planes of the wheel-tire system.
  • bearing 14 includes a hollow tubular portion extending rightwardly along shaft 12 and that the actual bearing surface is disposed at or about the end of tubular portion 15. This places the actual bearing support in substantial registration with the plane of the rim of wheel 20 as indicated by reference line 22.
  • This is also known as the inner edge of the wheel-tire system and is one plane of reference which, together with the plane represented by reference line 21, the outer plane (extending substantially within the plane of the right or outer rim of wheel 20) form two reference planes or surfaces in which weights may be deposited at appropriate angular positions to compensate for any imbalance in the wheel-tire system.
  • FIGS. 3, 4 and 5 are concerned with illustrating some details of the velocity and positioning portions of our invention.
  • Disk 27 is shown having apertures 28 on a common radius.
  • apertures 28 are disposed in 64 spaced apart locations whereby the angular distance between each of the apertures is 5 degrees, the resolution deemed desirable for establishing the radial position of an imbalance force and the position of the location on the object to be balanced for adding suitable material to compensate for the imbalance.
  • a further aperture 29 is disposed radially inwardly and is a single aperture. Referring to FIG.
  • radiation source 30 may be comprised of individual elements, for example, light emitting diodes that are appropriately positioned as in FIG. 3 and FIG. 4, the array may be considered to be, collectively, as shown on FIG. 1, as a source of radiation 30.
  • the sensors which may take the form of photoelectric transistors 31, 32 and 33, are disposed to coact with the apertures in disk 27 such that detector 33 is energized or illuminated once during each complete revolution of disk 27. Sensors 31 and 32 are spaced apart such that one of them may be on the center line of an aperture and the other one will have its center line at approximately one or the other edges of an aperture, as shown in FIG. 5.
  • This provides for signals from detectors 31 and 32 which, when properly processed, not only provide an angular position signal, but which may, and as described below, provide a direction of rotation signal which is utilized to properly process the angular positional information as well as to control the operation of motor 11. While it may, in some circumstances, be desirable to obtain rotational velocity information from sensors 31 and 32, a separate sensor 33 is utilized in combination with the electronic and electrical computing aspects of our invention under circumstances which, it has been discovered, a single informational signal is useful to indicate the rotational velocity of shaft 12.
  • windings 47 and 135, also indicated by reference characters F2 and F1 represent the output windings of the planar motion velocity detectors 25 and 26, respectively.
  • These sources of signals are also related to inner and outer planes 22 and 21 and the signal appearing at winding 47 is related related to the outer plane, while the signals appearing at 47 and 135 is related to the inner plane.
  • three light emitting diodes are shown in phantom form as suitably energized from a source of potential in the circuit which includes resistor 217.
  • Detectors 31, 32, and 33 are shown in the form of photoelectric transistors having their emitters connected in common to a source of potential and their collector electrodes each connected to amplifiers 220, 235 and 322, respectively.
  • inner and outer meters 35 and 34 are shown in phantom connection to the outputs of amplifiers 206 and 121, respectively, and to a common signal ground.
  • inner and outer indicator lamps 37 and 36 are shown connected to the outputs of transistors 305 and 312, respectively, and, through a phantom connection, to a source of potential. Further outputs are indicated as the motor contactor windings of motor 11, windings 354 and 365, representing forward and reverse operation of motor 11. Winding 354 is shown connected to the output of transistor 358 and winding 365 is shown connected to the output of transistor 364.
  • winding 47 has its lower end connected to a signal ground through resistor 50 and its upper end connected to input terminal on amplifier 52 through resistor 48 and capacitor 51.
  • a resistor 53 interconnects the input and output terminals on amplifier 52 and a further resistor 54 connects the output terminal to another input terminal.
  • the lower end of resistor 54 is connected to ground through capacitor 56 and to an input terminal on amplifier 58 through resistor 55 and potentiometer 57.
  • Another input terminal on amplifier 58 is connected to ground and the output terminal is connected to the other input terminal through potentiometer 60 and resistor 59.
  • the output terminal of amplifier 58 is connected to the input terminal on amplifier 63 through potentiometer 61 and resistor 62.
  • the output terminal on amplifier 63 is connected to the same input terminal through resistors 65 and 64 and the other input terminal is shown connected to ground.
  • the output terminal on amplifier 63 is connected to an input terminal on amplifier 68 through capacitor 66 and resistor 67. The same input terminal is connected to the output terminal on amplifier 68 through capacitor 70 and resistor 69, connected in parallel and the other input terminal is connected to ground.
  • the output terminal on amplifier 68 is connected to an input terminal on amplifier 74 through potentiometer 71 and resistor 73. The output terminal is connected to the same input terminal through the parallel combination of capacitor 75 and resistor 76. The other input terminal is connected to ground.
  • the output terminal on amplifier 74 is connected to an input terminal on amplifier 79 through capacitor 77 and resistor 78.
  • a further resistor 80 connects the output terminal with the same input terminal and the other input terminal is shown connected to ground through resistor 81.
  • the output of amplifier 79 is connected to a full-wave demodulator which includes amplifiers 85 and 94.
  • the output of amplifier 79 is connected to the input of amplifier 85 through capacitor 82 and resistor 84.
  • the input terminal is also connected to the output terminal on amplifier 85 through diode 88, resistor 90 and diode 87.
  • the other input terminal on amplifier 85 is connected to ground and intermediate contacts 1 and 4 are interconnected through capacitor 86.
  • the junction of capacitor 82 and resistor 84 is connected to an input terminal on amplifier 94 through resistor 92.
  • the same input terminal is also connected to the output terminal through resistor 97. Further, the input terminal is connected to the junction between resistor 90 and diode 87 through resistor 93.
  • the other input terminal is connected to ground through resistor 95 and terminals 4 and 8 are interconnected by capacitor 96.
  • the demodulated signal appearing at the output terminal of amplifier 94 is connected to a filtering network comprised of resistors 99 and 101 to an input terminal on amplifier 102, the input terminal is also connected to ground through capacitor 103.
  • the other input terminal on amplifier 102 is connected to its output terminal and to the junction between resistors 99 and 101 through capacitor 100.
  • the output terminal on amplifier 102, a well-filtered dc potential can be applied to an input terminal on amplifier 121 through analogue switch 104 and conductor 105 for purposes of calibration.
  • the output terminal on amplifier 102 is also connected to an input terminal on amplifier 108 which functions as a voltage comparator.
  • the output of voltage comparator 108 is connected to an input terminal on flip-flop 113 through resistor 111 and resistor 112. The output of voltage comparator 108 is also connected to another input terminal through resistor 104.
  • the output terminal on flip-flop 113 is connected to the enable terminal on the left hand section of binary counter 118 to enable it to receive clock pulses through its No. 1 terminal from the output of gate 232.
  • the output terminals on binary counter 118 are connected to the input terminals on a resistor network 119 which converts the binary signals into an analog potential.
  • the output terminals are also connected to nand gate 117 which is in turn connected to the reset terminal on flip-flop 113 through inverter 116 and diode 114.
  • the output terminal on resistor network 119 is connected to amplifier 121 and to ground through resistor 120.
  • a further input terminal is connected to the output terminal of amplifier 121.
  • the output terminal of amplifier 121 is connected to meter 34 through resistor 123 and to ground through diode 122.
  • the output terminal is further connected to an input terminal on amplifier 128 through resistor 124.
  • the same input terminal is connected to the output terminal of amplifier 128 through resistor 129 and to a source of potential through resistors 127 and 125 and to ground through resistor 127 and diode 126.
  • the output of amplifier 128 is connected to the input of amplifier 131 through resistor 130.
  • the same input terminal is connected to the output terminal of amplifier 131 through capacitor 132 having a resistor 133 in parallel therewith.
  • the other input terminal is connected to ground.
  • the output terminal of amplifier 131 is connected to the lower input terminal on amplifier 108 through resistor.
  • the output winding 135 on velocity transducer 26 is connected to inner meter 35 through amplifier 140, amplifier 148, amplifier 150, amplifier 160, potentiometer 72, amplifier 164, amplifier 167, demodulator 173 and 181, amplifier 189, voltage comparator 374, flip-flop 380, digital counter 203-204, resistor network 205 and amplifier 206.
  • the output of amplifier 206 is connected to voltage comparator 374 through amplifiers 211 and 214, and the output of digital counter 203-204 is connected to the reset terminal on flip-flop 380 through nand gate 202 and amplifier 201.
  • the output of the resistor network 119 is connected to the output terminal of amplifier 102 through conductor 105 and flip-flop 104.
  • the output of resistor network 205 is connected to the output terminal of amplifier 189 through flip-flop 191.
  • an interconnection between the two signal processing paths shows the output of amplifier 58 connected to the input of amplifier 150 through resistor 151, amplifier 152 and resistor 154.
  • the output terminal of amplifier 152 is also shown connected to the input terminal that is connected to resistor 151.
  • the other input terminal is connected to ground.
  • FIGS. 6B, 6D, 6E and 6G the left hand end of FIG. 6B represents the signals received from disk 27 and its adjacently disposed sources of illumination 30 and radiation responsive signal generating elements shown in the form of transistors 31, 32 and 33.
  • the light emitting diodes D, C and R are energized from the power supply (not shown) from the negative terminal through the diodes to a ground terminal through resistor 217.
  • the output of transistor 31 is connected to an input terminal on amplifier 220.
  • the input terminal is connected intermediate positive and negative terminals on the power supply (not shown) through resistors 214 and 218.
  • the other input terminal on amplifier 220 is connected to its output terminal through resistor 222 and to ground through resistor 221.
  • the output of amplifier 220 is connected to input terminals on nand gates 227 and 228 through resistor 223.
  • the output terminal on amplifier 220 is also connected to the voltage source through resistor 224.
  • the output of transistor 32 is connected to an input terminal on amplifier 235 which is in turn connected to positive and negative sources of voltage (not shown) through resistors 233 and 234, respectively.
  • the output terminal of amplifier 235 is connected to another input terminal through resistor 237 and to ground through resistor 236.
  • the outputof amplifier 235 is connected to inverter 240 through resistor 238 and to a source of voltage through resistor 239.
  • the output of inverter 240 is connected to an input terminal flip-flop 226 and to the input of phase lock loop 254.
  • Flip-flop 226 also has a clock terminal connected to an oscillator comprised of amplifiers 241 and 244.
  • the input terminals of amplifier 241 are connected to its output terminal and the output terminal of amplifier 244 through resistor 242 and resistor 243 and capacitor 245, respectively.
  • the output terminal on amplifier 241 is connected to an input terminal on amplifier 244, the output terminal of which is connected to the clock terminal indicated by 3 on flip-flop 226, and to the clock terminal indicated by 11 on flip-flop 225.
  • the Q terminal on flip-flop 226 is connected to an input terminal on nand gate 228.
  • the Q terminal on flip-flop 226 is connected to the D or drive terminal on flip-flop 225.
  • the Q terminal on flip-flop 225 is connected to an input terminal on nand gate 227 and the Q terminal on flip-flop 225 is connected to an input terminal on nand gate 228.
  • the oscillator connected to the clock terminals on flip-flop 225 operates at a substantially higher, in the order of ten times or more higher, frequency than the signals which are generated by disk 27 through its apertures 28 to transistors 31 and 32.
  • the output of nand gate 227 is connected to input terminals on nand gates 229 and 231 and the output of nand gate 228 is connected to input terminal on nand gate 230 and an input terminal on nand gate 231.
  • the output of nand gate 229 is connected to an input terminals on nand gate 230 and nand gate 231.
  • the output of nand gate 230 is connected to an input terminal on nand gate 229 and to the up-down direction terminals 10 on up-down counters 273 and 272.
  • nand gate 231 The output of nand gate 231 is connected to count terminals 15 on binary counters 273 and 272, respectively, through nand gate 232, and to the clock terminals 1 on binary counters 118 and 203.
  • the outputs Q4, Q3, Q2 and Q1 on up-down counter 272 are connected to inputs D4, D3, D2 and D1 on hex latches 277 and 278.
  • Output terminals Q6 and Q5 on up-down counter 273 are connected to input terminals on exclusive or gates 275 and 274, respectively, and further to input terminals on the indicated exclusive or gates connected to the output of hex latches 277 and 278.
  • the output of exclusive or gate 275 is connected to input terminals D4 on hex latches 277 and 278 and to an input terminal on exclusive or gate 274.
  • the output of exclusive or gate 274 is connected to an input of exclusive or gate 276 and to terminals D6 on hex latches 277 and 278.
  • the output terminals of hex latches 277 and 278 are connected to input terminals of certain ones of the exclusive or gates appearing adjacent the right sides of hex latches 277 and 278 with the connections performed as indicated.
  • the outputs of the exclusive or gates are connected to a pair of nor gates and thence to nand gates 280 and 279, respectively.
  • the output of nor gate 280 is connected to an input terminal of a nand gate 289, the output of which is connected to inner indicator lamp 37 through resistor 300 having diode 301 in parallel therewith, the input terminal of amplifier 306, such input terminal also being connected to ground through capacitor 302, resistor 303 and transistor 305 through indicator 37 to a source of negative potential (not shown).
  • the output of nand gate 279 is connected to an input terminal of nor gate 290, the output of which is connected to outer indicator 36 through resistor 308 having diode 307 in parallel therewith, the input terminal of amplifier 309, such input terminal being connected to ground through capacitor 310, resistor 311 and transistor 312.
  • the count terminal 9 on hex latches 277 and 228 is controlled from flip-flops 287 and 335, respectively. These are in turn controlled from a signal derived from the zero crossing of the velocity signal appearing in the inner and outer channels which correspond to the positional information that is to be processed for the inner and outer channels.
  • Flip-flop 287 is connected to the inner channel at the output of amplifier 167 through conductor 170 connected to an input terminal of amplifier 256, the output of which is connected to the C terminal of flip-flop 287 through resistor 284.
  • the C terminal is also shown connected to a source of voltage through resistor 275.
  • the output of amplifier 256 is connected to an input terminal through resistor 283 and to ground through resistor 282.
  • flip-flop 335 is connected to the output of amplifier 79 through conductor 83, resistor 330 connected to an input terminal on amplifier 229 and resistor 333.
  • the C terminal on flip-flop 335 is also connected to a source of potential through resistor 334 and the output terminal on amplifier 229 is connected to an input terminal through resistor 332 and to ground through resistor 331.
  • an oscillator comprised of a multivibrator 250 is shown having resistors 252 and 253 intermediate its terminals 2 and 3 and a capacitor, 254, connected between terminals 1 and 3 and other terminals connected to either a source of voltage or to ground.
  • the output is applied to a phase locked loop which is shown having its output connected to ground through resistor 255 and to amplifier 260 through resistor 256 and 257. That the input terminal on amplifier 260 is also connected to ground through capacitor 259.
  • the junction between resistors 256 and 257 is connected to a further input terminal on amplifier 260 through a capacitor 258 and that input terminal and output terminal are shown interconnected.
  • the output of amplifier 260 is connected to the input of amplifier 263 through resistor 261 and to a source of negative potential through resistor 262.
  • the other output terminal of amplifier 263 is shown connected to ground through resistor 264 and to its output terminal through resistor 265.
  • a further resistor 266 is shown connecting the output of amplifier 263 to one of the terminals on single pole double throw switch 268.
  • the same terminal on switch 268 is also connected to a source of positive potential through resistor 267. In the run position of switch 268, the output of amplifier 263 is applied to input terminal C A of binary counter 270.
  • transistor 33 is shown having its output connected to an input terminal on amplifier 322 and to positive and negative sources of voltage through resistors 320 and 321, respectively.
  • Another input terminal on amplifier 322 is connected to ground through resistor 323 and to the output terminal through resistor 324.
  • the output of amplifier 322 is connected to the E A terminal on binary counter 270.
  • the right end of resistor 325 is connected to a positive source of potential through resistor 326 and to ground through capacitor 327.
  • the Q5 and Q1 outputs of binary counters 270 and 271, respectively, are connected to the input terminals of nand gate 328.
  • One of the input terminals (6) of nand gate 328 is connected to the 5 and 9 terminals of flip-flops 335 and 287, respectively, and to the clock terminals 3 and 11 on flip-flops 113 and 148, respectively.
  • the output terminal of nand gate 328 is connected to an input terminal on nand gate 349 through a capacitor 339, the other input of nand gate 349 is connected to the output of nand gate 293 through resistor 348 and to an input terminal on nand gate 294.
  • the output of amplifier 353 is connected to the forward winding on motor 11 through resistor 356 having capacitor 355 and resistor 357 in parallel therewith through transistor 358 connected to a source of potential (not shown) to the winding.
  • the output of amplifier 353 is also connected to the count terminal on flip-flop 357.
  • Flip-flop 357 is shown with its reset terminal at the lower bottom connected through a resistor 172 to the output of an inverter 171 and to the output of nor gate 170.
  • the Q terminal on flip-flop 357 is connected to the reverse motor winding 365 through amplifier 360, having its output connected to the Q terminal on flip-flop 357 and to transistor 364 through resistor 363 having capacitor 361 and 362 in parallel therewith and having an emitter terminal connected to a source of potential (not shown).
  • a pair of NAND gates 291 and 292 are shown having their output terminals interconnected to the respective input terminals and the other input terminals connected across resistors 297 and 298 which are connected to the start-stop switch at the bottom of FIG. 6G to be alternately connected to ground.
  • the mid-points of resistors 297 and 298 are connected to a source of potential (not shown)
  • the output of NAND gate 292 is connected to the count terminal on flip-flop 352 and the lower terminal on nor gate 170 and the output terminal on nand gate 291 is connected to the reset terminals on hex counters 277 and 278.
  • an exclusive or gate 340 having one input terminal connected to ground and the other input terminal connected to ground through capacitor 342 and to a source of potential (not shown) through resistor 341.
  • the output of exclusive or gate 340 is connected to the base electrode of transistor 346 through resistor 243 and to the emitter and a source of positive potential (not shown) through resistor 344.
  • the collector of transistor 346 is connected to ground through resistor 345 and, through diode 288, to the reset terminals on flip-flops 287 and 335, the reset terminals are A and b on binary counters 270 and 271 and to the reset terminals on binary counters 118, 203 and 204; and to the reset terminals on flip-flops 352 and 357 through diodes 351 and 173, respectively; and to the reset terminals on flip-flops 113 and 148 through diodes 115 and 146, respectively.
  • the following is a table of values of components used in the fabrication of the illustrative embodiment:
  • the rim width is determined and potentiometer 61, having previously been calibrated in units of rim width, is adjusted as well as rim diameter potentiometers 71 and 72, which likewise have been calibrated in terms of units of diameter for the wheel, are likewise adjusted so that the computations performed relative to the magnitudes of the forces of unbalance may be directly read on meters 34 and 35 in units of weight of material to be added at predetermined angular positions on the rim of the wheel-tire system.
  • Oscillator 250 is energized and operative to oscillate at a frequency related to the desired velocity of revolution of shaft 12, as determined by the number of apertures 28 in disk 27, its output is connected to phase lock loop 254 which results in no output at switch 268. Further, the high frequency, in the magnitude of ten times the frequency of oscillator 250, oscillator is energized to continuously clock flip-flops 225 and 226 (FIG. 6B). Further, the output of flip-flop 352 on FI. 6G is of a polarity as to inhibit the operation of nor gates 289 and 290 so that no output therefrom will be applied to inner and outer indicators 37 and 36 (FIG. 6G). There are no signals applied to any of the input channels shown at the left end of FIG. 6A and 6B for the magnitude-force and phase and frequency sources of signal.
  • the apparatus is in readiness for the determination of the amount of unbalance and the necessary action to be taken by the operator as far as adding weights at predetermined locations in the two planes of rotation of wheel-tire system 20-23; namely, at the rim of the wheel 20 at the angular positions to be determined.
  • the operator initiates the operation by momentarily reversing the contacts on the start-stop button shown at the lower left hand end of FIGS. 6G.
  • This results in the application of a pulse to the C terminal of flip-flop 352 from nand gate 292 which in turn results in a Q output which, when conveyed through inverter 353 to transistor 358 results in the energization of motor forward drive winding 354.
  • an inhibit pulse is transmitted from the Q terminal of flip-flop 352 to NOR gates 289 and 290 for inhibiting the application of any output to inner and outer indicators 37 and 36.
  • nand gate 291 to the reset terminals on hex counters 277 and 278 places them in condition for registering and storing information concerning the angular positions of shaft 12.
  • the reversal of the state of the multivibrator comprised of nand gates 293 and 294 in the lower left hand corner of FIG. 6G results in a removal of the reset signal from nand gate 349 to reset terminal 10 on flip-flop 352.
  • the forward winding of motor 10 is thus energized and motor 10 is operative to initiate and accelerate the rotational speed of shaft 12.
  • phase lock loop 259 will become operative to transmit the oscillator signal as a clock to the timing circuit comprised of binary counters 270 and 271 which is enabled once a revolution by the velocity of rpm signal supplied from photoelectric transistor 33, such signal is also supplied to up-down counters 273 and 272, to reset the counters at the beginning of every revolution of operation of shaft 12.
  • binary counter 270 continues to receive an enabling signal once every revolution so that it may accept clock pulses from oscillator 250 to continue its counting operations and up-down counters 273 and 272 are reset at the beginning of every revolution by the signals determined from photoelectric transistor 33 in response to aperture 29 in disk 27.
  • flip-flops 225 and 226, and nand gates 227 and 228 and 231 and 232 will be operative to provide the counting pulse train to counters 273 and 272, the outputs of which are combined to form a code which is applied to the inputs of hex latches 277 and 278 to thereby control the respective output terminals indicated by Q1, Q6.
  • the output of the hex latches which continuously step up and down in accordance with the signals provided from up-down counters 273 and 272, and which continue to change as shaft 15 rotates, are connected, in each case, to a plurality of logic elements shown in the form of exclusive or gates, nor gates, and each culminating in a hand gate 280 and 279, respectively, the output of which may be used to activate inner and outer indicators 37 and 36, respectively.
  • indicators 37 and 36 are each energized through a fast-on, slow-off network including resistor 300, diode 301, capacitor 302 and inverter 306, in the case of the "inner" channel.
  • the signals applied to the outer and inner channels appearing at FIG. 6A, FIG. 6E, and FIG. 6F first proceed, in the case of both channels, through a zero phase shift signal processing portion of the channels up to capacitors 92 and 171, respectively, at which point they are still in the form of alternating potentials which have a magnitude corresponding to the degree of velocity of unbalance for any given angular position of shaft 12 as an instantaneous signal.
  • the inner channel's signal is modified by the introduction of selected portions of the outer channel signal through amplifier 152 and the interconnection between the output of amplifier 63 and amplifier 150.
  • the signals After the signals have been thus processed, they are each demodulated and filtered to provide a dc level corresponding to the magnitude of the maximum unbalance of the wheel-tire system. These signals are compared in comparators 108 and 142, the output of which is applied to binary counters 118 and 203-204, respectively. The counters continue to operate according to the frequency of the clock signal applied from the output of nand gate 232 (corresponding to the angular outer and inner meters 34 and 35 will reflect the average level of the force unbalance signals as determined by the displacement of bearings 13 and 14 from their normal positions).
  • hex latches 277 and 278 and the associated logic connected to their respective outputs and the logic associated with the outputs of up-down counters 273 and 272 is such that by using the connections indicated (only some of which are shown as complete conductors) a 90° phase shift is computed into the operation of the counters for the logic associated with the hex latches so that when a real time positional signal is present in the hex latches, the logic consisting of the exclusive or and nor gates connected between hex latches 277 and 278 and nand gates 280 and 279, respectively, will respond to a particular count with a 90° shift.
  • the hex latches will operate continuously to store the signals applied to them until the first zero crossing of the signals appearing at amplifiers 79 and 167 at which time flip-flops 287 and 335 are toggled by zero crossing detectors 256 and 229 to "latch" hex latches 277 or 278 to store the signal appearing therein at that instant. This signal will be available for the illumination of indicators 37 or 36 in subsequent phases of operation of the machine.
  • nand gate 328 transmits a signal to nand gate 349 which resets flip-flop 352 to de-energize motor forward winding 354, removes the inhibit signal from nor gates 289 and 290 and supplies a pulse to toggle flip-flop 357 to energize motor reverse winding 365.
  • flip-flops 113 and 148 have been toggled by the operation of comparators 108 and 142 in driving binary counters 118 and 203-204 to a condition which supplies an output voltage through digital to analog converters 119 and 205 so that the energization of meters 34 and 35, calibrated in convenient units, will indicate the correct total of weight to be supplied to the inner and outer planes of rotation of the wheel-tire system.
  • the energization of reverse winding 365 serves to provide a rapid braking of motor 11 and when a signal that is derived from the positional information derived from apertures 28 on disk 27, appears at the output of nand gate 229 and to nor gate 170 to the reset terminal on flip-flop 357 to thereby de-energize motor reverse winding 365 and the system is at rest.
  • the same signal is also applied to the reset terminals on flip-flops 287 and 335 through resistor 336 (FIG. 6E), to reset terminals 7 and 15 on binary counters 270 and 271 and to the reset terminals on binary counters 118 and 203-204 and the previously described operation ensues.
  • the motor rapidly brings the wheel and tire system up to the predetermined speed and maintains the speed for sufficient time to enable the measurement functions to be completed (this need only be a few revolutions in actual practice), and then brings the motor to a rapid stop to allow the operator to complete the balancing operation by the application of weights at the appropriate locations in the amount indicated.
  • One of the features of our invention is concerned with the provision of a means for measuring angular position and direction of rotation with the utilization of a plurality of apertures spaced at angular positions chosen to provide the revolution necessary for effecting a satisfactory balancing of the wheel-tire system.
  • 64 apertures 28 were disposed on a common radius around the periphery of disk 27.
  • a pair of sources of radiation 30, which may take the form of light emitting diodes, were disposed at the same angular spacing and a pair of photoelectric transistors 31 and 32 were disposed with the center axis of transistor 31 and the center axis of transistor 32 angularly spaced a distance somewhat less than the center axes of the equally spaced apertures 28.
  • nand gate 229 whenever the disk is running in a reverse direction and an output from nand gate 232 whenever the disk is running in a forward direction, the total number of pulses being equal to the total number of apertures for the angular revolution required.
  • the clock in the forward direction provided for up-down counters 273 and 272 and for binary counters 118 and 203-204 consists of 64 pulses per revolution at a constant frequency when the motor is driving shaft 11 at the desired speed.
  • test functions associated with switch 169 on the lower right hand corner of FIG. 6B and the switch and functions associated with analogue switch 104 and 191 at the top of FIG. 6C are not essential to the operation of our invention and therefore the description and operation of same are not included.

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Testing Of Balance (AREA)

Abstract

This invention is directed to an off-the-vehicle type of wheel-tire balancer for vehicular wheels. A wheel and tire assembly which is to be balanced is disposed on a rotating shaft under the control of a signal responsive electronic control apparatus utilizing rotational velocity signals, rotational, directional, and positional signals and velocity of displacement of the mounting apparatus for the shaft to provide a suitably calibrated indicators, the amount of weight to be added at certain angular positions on the inner and outer planes of the wheel rim to provide a dynamic balance of the wheel-tire system. Further indicators are provided for relating the indicated weight to be added to an angular position of the wheel and tire system. The entire apparatus is automatic in operation in that once the system is started, a motor is energized to rapidly rotate the wheel-tire system up to a predetermined rotational velocity. Once this is attained, the magnitude and angular disposition of the weights to be disposed on the rims of the wheel-tire system is rapidly detected over but a few revolutions of the shaft and following this, the motor is energized in a reverse direction to provide a dynamic breaking force to rapdily bring the wheel-tire system to a rest position, the energization of the motor in the reversed direction being maintained until the shaft is actually reversed its direction of rotation for a predetermined angular displacement.

Description

BACKGROUND OF THE INVENTION
The prior art with which this invention is concerned contains numerous examples of apparatus and concepts for balancing the wheel-tire systems of a vehicle so as to eliminate destructive and annoying vibrations present at various resonant frequencies of operation caused by static and dynamic imbalances in a wheel-tire system for each of the wheels of a vehicle.
For various reasons, including manufacturing inconsistencies, the majority of the wheel-tire systems on vehicles have imbalances which are not only annoying, but actually lead to premature failure of the tires and of the other components of the suspension systems for such vehicles.
It has been determined that one concept for determining the location and weight of materials to be added to a wheel-tire system should employ a dynamic measurement of the imbalance at one or more predetermined frequencies or rotational speeds of operation of the wheel-tire system. One of these have attempted to make the corrective determination while the wheel-tire system is in place on the suspension system of a vehicle thereby "tuning" the entire system. Such equipment has proven unsuitable under many conditions of operation and therefore, while such apparatus is available, it is the opinion of the inventors of the subject matter of this system that physically removing a wheel-tire system and providing a dynamic balance for each of the wheels of a vehicle provides uncomplicated, efficient and satisfactory dynamic balance of a wheel-tire system for each of the wheels of the vehicle.
SUMMARY OF THE INVENTION
The present invention facilitates that balancing of a wheel-tire system by providing an operation whereby the wheel-tire system is mounted upon a shaft that is in turn driven by a motor that is under the control of a system which accepts signals generated by the shaft and its mountings whereby a wheel-tire system is disposed on the shaft and a motor is energized to impart rotation to the shaft and wheel-tire system. Predetermined frequency or angular velocity of the shaft is selected in accordance with the intended operational characteristics of the vehicle upon which the wheel-tire systems are to be used. Sources of signal corresponding to the rotational velocity or speed of the shaft and the angular position of the shaft, resolved to a predetermined angular degree, are utilized to first detect the coincidence of actual speed with predetermined speed for the shaft at which time both of the signals corresponding to speed and angular position are utilized to process the information derived from two or more sources of signal that are responsive to the velocity of displacement of the shaft in a plane. The processing of the information contained in the signals continues for a short predetermined time after which, the motor is energized in such a manner to cause reverse operation and this form of dynamic braking of the motor, which takes place over a very short period of time, brings the wheel-tire system to a rapid stop position, such position being related to the reverse direction of the shaft for a predetermined, short angular motion. The magnitudes of the weights relating to the imbalance of the wheel-tire system may conveniently be displayed on meters calibrated in ounces or grams or other suitable systems of weight measure. In addition to the magnitudes, there are provided further signal responsive means which will energize an indicator such as a lamp, whereby when the wheel-tire system is rotated on the shaft, an angular position for each of the magnitudes of corrective weights will be indicated by illumination of the lamp or other indicator, the angular position being related to the magnitudes and each being related to one of the planes of the wheel that is adjacent the rims, such planes lying in perpendicular disposition with respect to the axis of rotation of the shaft upon which the wheel-tire system is mounted.
It is therefore an object of our invention to provide an accurate and efficient off-the-vehicle wheel and tire system balancing apparatus. Other objects and advantages of our invention will become apparent from a consideration of the appended specification, claims, and drawings in which:
FIG. 1 is a schematic and diagrammatic representation of an operational system embodying the principles of our invention;
FIG. 2 is a side elevational view, partly in section, of a portion of the right end of FIG. 1 showing the relationship between a bearing and a wheel mounted on the shaft;
FIGS. 3, 4 and 5 are detailed views showing the relationship of the elements disposed on the left end of FIG. 1 of the drawings; and
FIGS. 6-6G comprise an electrical schematic diagram incorporating the principles of my invention into a signal processing and motor control system as embodied on FIG. 1 of the drawings, specifically, FIG. 6 illustrates the manner in which FIGS. 6A-6G may be assembled to form a complete electrical and diagrammatic showing of our invention.
DETAILED DESCRIPTION OF THE DRAWINGS
Referring to FIG. 1 of the drawings, a diagrammatic representation of a complete balancing machine is indicated generally by reference character 10. The apparatus includes a rotatable shaft 12 having an axis of rotation 12A. A pulley 17 is nonrotatably disposed on shaft 12 and is driven by motor 11 having an output pulley 18 through drive belt 19. Shaft 12 is rotatably journaled in bearings 13 and 14, such bearing being mounted upon a suitable base whereby forces that may be exerted thereon due to an imbalance in a wheel-tire system 20-23, are constrained and do in fact occur substantially within a plane, as indicated by reference character 16. The velocity of the back and forth movement of bearings 13 and 14 within plane 16 may be sensed by suitable velocity detecting transducers 25 and 26 which serve to convert any displacement of bearings 13 and 14, along the directions indicated adjacent them into electrical signals that are representative of such velocity of displacement. A wheel-tire assembly is shown disposed on the right end of shaft 12 by suitable screw threaded means that may be attached to the mounting holes on wheel 20, such mounting is indicated by reference character 24, and as will be discussed below, mounting member 24 is adjustable longitudinally of shaft 12 to provide positioning of one of the planes of rotation of wheel-tire system 20-23 in the plane of rotation of one of the effective portions of one of the bearing members. A position and speed signal generator, indicated by reference character 27, includes a plurality of apertures 28 disposed on a common radius and at intervals sufficiently small to provide the required angular resolution of a shaft position during the balancing operations. A further single aperture 29 is shown disposed on a different radius and, as will be explained in more detail below, serves to provide a signal proportional to the rotational velocity of shaft 12. Suitable sources of light, disposed in predetermined relationship with apertures 28 and 29 in signal generating member 27, are provided to illuminate a plurality of light sensitive sources of signal indicated by reference characters 31, 32, and 33. Each of these is shown connected through suitable conductors 40, 41, and 42, respectively, to a signal processor and motor control, block. Similarly, motor 11 is connected to the same block through conductor 45 as are the outputs of velocity of displacement sensors 25 and 26 through conductors 43 and 44, respectively. A pair of indicating lamps 36 and 37, further identified by φI and φO, and a pair of indicating meters 34 and 35 are likewise indicated by WO and WI.
In operation, briefly, a wheel-tire system is suitably disposed on mounting clamp 24 and the assembly is locked in place with the plane of rotation of the inner rim of wheel 20 in the plane of rotation of the effective bearing portion of bearing 14 (as seen on the left end of portion 15 of bearing 14). Signal processor and motor control may be operable to initiate operation of the system of energizing motor 11 to drive shaft 12 in a predetermined direction. As shaft 12 reaches a predetermined rotational velocity, signal processor and motor control block becomes operative to accept the velocity of displacement signals from sensors 25 and 26 and the velocity and position of rotation as determined through the use of sensors 31, 32 and 33, to make a rapid determination of the amount of weight that is necessary to correct the imbalance of the wheel-tire system and the angular positions that the weights should be added to the wheel-tire system, after which motor 11 is de-energized and then re-energized in a reverse direction to rapidly effect a dynamic breaking of shaft 12 and, upon detection of the reverse revolution of shaft 12 over the predetermined degrees of angular resolution, it would de-energize motor 11 and allow the shaft to remain at rest. At this time, meters 35 and 34 indicate the amount of weight to be added to the wheel and tire systems on the inner plane 22 and outer plane 21. Indicators 37 and 36 are energized at this time. In order to complete the balancing operation, the operator manually rotates the wheel-tire system and at the position that the weight is required as indicated on meters 35 and 34, one or the other of indicators 37 and 36 will be energized to indicate to the operator that the correct angular position for adding the weight has been reached. Conveniently, one might use a vertical axis through generally horizontal plane 16 as a reference so that the operator will know where to attach the indicated corrective weight to each of the planes of the wheel-tire system. In other words, there need be no angular scale or other forms of indicia required, the location at which the weight is applied with respect to plane 16 remains constant while the wheel is rotated on shaft 12 and when the appropriate angular position is obtained, the appropriate indicator light will alert the operator that a weight should be attached at that particular angular position of wheel 20.
Referring to FIG. 2 of the drawings, it may be seen that bearing 14 includes a hollow tubular portion extending rightwardly along shaft 12 and that the actual bearing surface is disposed at or about the end of tubular portion 15. This places the actual bearing support in substantial registration with the plane of the rim of wheel 20 as indicated by reference line 22. This is also known as the inner edge of the wheel-tire system and is one plane of reference which, together with the plane represented by reference line 21, the outer plane (extending substantially within the plane of the right or outer rim of wheel 20) form two reference planes or surfaces in which weights may be deposited at appropriate angular positions to compensate for any imbalance in the wheel-tire system.
Before proceeding into a detailed description of the electrical schematic and diagrammatic portion of this invention, reference is made to FIGS. 3, 4 and 5 which are concerned with illustrating some details of the velocity and positioning portions of our invention. Disk 27 is shown having apertures 28 on a common radius. For the purposes of the present disclosure, apertures 28 are disposed in 64 spaced apart locations whereby the angular distance between each of the apertures is 5 degrees, the resolution deemed desirable for establishing the radial position of an imbalance force and the position of the location on the object to be balanced for adding suitable material to compensate for the imbalance. A further aperture 29 is disposed radially inwardly and is a single aperture. Referring to FIG. 3, it may be seen that radiation source 30 may be comprised of individual elements, for example, light emitting diodes that are appropriately positioned as in FIG. 3 and FIG. 4, the array may be considered to be, collectively, as shown on FIG. 1, as a source of radiation 30. The sensors, which may take the form of photoelectric transistors 31, 32 and 33, are disposed to coact with the apertures in disk 27 such that detector 33 is energized or illuminated once during each complete revolution of disk 27. Sensors 31 and 32 are spaced apart such that one of them may be on the center line of an aperture and the other one will have its center line at approximately one or the other edges of an aperture, as shown in FIG. 5. This provides for signals from detectors 31 and 32 which, when properly processed, not only provide an angular position signal, but which may, and as described below, provide a direction of rotation signal which is utilized to properly process the angular positional information as well as to control the operation of motor 11. While it may, in some circumstances, be desirable to obtain rotational velocity information from sensors 31 and 32, a separate sensor 33 is utilized in combination with the electronic and electrical computing aspects of our invention under circumstances which, it has been discovered, a single informational signal is useful to indicate the rotational velocity of shaft 12.
Referring to composite FIG. 6-6G, it may be seen at the right-hand portions of FIGS. 6A and 6B that the signals referred to above are presented at the inputs to the electrical and electronic portions of the balancing apparatus. On FIG. 6A, windings 47 and 135, also indicated by reference characters F2 and F1, represent the output windings of the planar motion velocity detectors 25 and 26, respectively. These sources of signals are also related to inner and outer planes 22 and 21 and the signal appearing at winding 47 is related related to the outer plane, while the signals appearing at 47 and 135 is related to the inner plane. At the left end of FIG. 6B, three light emitting diodes are shown in phantom form as suitably energized from a source of potential in the circuit which includes resistor 217. Detectors 31, 32, and 33 are shown in the form of photoelectric transistors having their emitters connected in common to a source of potential and their collector electrodes each connected to amplifiers 220, 235 and 322, respectively. At the right-hand end of FIGS. 6F and 6G, inner and outer meters 35 and 34 are shown in phantom connection to the outputs of amplifiers 206 and 121, respectively, and to a common signal ground. At the right end of FIG. 6G, inner and outer indicator lamps 37 and 36 are shown connected to the outputs of transistors 305 and 312, respectively, and, through a phantom connection, to a source of potential. Further outputs are indicated as the motor contactor windings of motor 11, windings 354 and 365, representing forward and reverse operation of motor 11. Winding 354 is shown connected to the output of transistor 358 and winding 365 is shown connected to the output of transistor 364.
Referring to FIGS. 6A, C and F, it may be recognized that there are essentially two channels for signal processing of the signals indicative of the velocity of displacement of bearings 13 and 14 as sensed by velocity detectors 25 and 26. The top or upper channel is as follows; winding 47 has its lower end connected to a signal ground through resistor 50 and its upper end connected to input terminal on amplifier 52 through resistor 48 and capacitor 51. A resistor 53 interconnects the input and output terminals on amplifier 52 and a further resistor 54 connects the output terminal to another input terminal. The lower end of resistor 54 is connected to ground through capacitor 56 and to an input terminal on amplifier 58 through resistor 55 and potentiometer 57. Another input terminal on amplifier 58 is connected to ground and the output terminal is connected to the other input terminal through potentiometer 60 and resistor 59. The output terminal of amplifier 58 is connected to the input terminal on amplifier 63 through potentiometer 61 and resistor 62. The output terminal on amplifier 63 is connected to the same input terminal through resistors 65 and 64 and the other input terminal is shown connected to ground.
The output terminal on amplifier 63 is connected to an input terminal on amplifier 68 through capacitor 66 and resistor 67. The same input terminal is connected to the output terminal on amplifier 68 through capacitor 70 and resistor 69, connected in parallel and the other input terminal is connected to ground. The output terminal on amplifier 68 is connected to an input terminal on amplifier 74 through potentiometer 71 and resistor 73. The output terminal is connected to the same input terminal through the parallel combination of capacitor 75 and resistor 76. The other input terminal is connected to ground. The output terminal on amplifier 74 is connected to an input terminal on amplifier 79 through capacitor 77 and resistor 78. A further resistor 80 connects the output terminal with the same input terminal and the other input terminal is shown connected to ground through resistor 81. The output of amplifier 79 is connected to a full-wave demodulator which includes amplifiers 85 and 94. The output of amplifier 79 is connected to the input of amplifier 85 through capacitor 82 and resistor 84. The input terminal is also connected to the output terminal on amplifier 85 through diode 88, resistor 90 and diode 87. The other input terminal on amplifier 85 is connected to ground and intermediate contacts 1 and 4 are interconnected through capacitor 86. The junction of capacitor 82 and resistor 84 is connected to an input terminal on amplifier 94 through resistor 92. The same input terminal is also connected to the output terminal through resistor 97. Further, the input terminal is connected to the junction between resistor 90 and diode 87 through resistor 93. The other input terminal is connected to ground through resistor 95 and terminals 4 and 8 are interconnected by capacitor 96. The demodulated signal appearing at the output terminal of amplifier 94 is connected to a filtering network comprised of resistors 99 and 101 to an input terminal on amplifier 102, the input terminal is also connected to ground through capacitor 103. The other input terminal on amplifier 102 is connected to its output terminal and to the junction between resistors 99 and 101 through capacitor 100. The output terminal on amplifier 102, a well-filtered dc potential can be applied to an input terminal on amplifier 121 through analogue switch 104 and conductor 105 for purposes of calibration. The output terminal on amplifier 102 is also connected to an input terminal on amplifier 108 which functions as a voltage comparator.
The output of voltage comparator 108 is connected to an input terminal on flip-flop 113 through resistor 111 and resistor 112. The output of voltage comparator 108 is also connected to another input terminal through resistor 104. The output terminal on flip-flop 113 is connected to the enable terminal on the left hand section of binary counter 118 to enable it to receive clock pulses through its No. 1 terminal from the output of gate 232. The output terminals on binary counter 118 are connected to the input terminals on a resistor network 119 which converts the binary signals into an analog potential. The output terminals are also connected to nand gate 117 which is in turn connected to the reset terminal on flip-flop 113 through inverter 116 and diode 114. The output terminal on resistor network 119 is connected to amplifier 121 and to ground through resistor 120. A further input terminal is connected to the output terminal of amplifier 121. The output terminal of amplifier 121 is connected to meter 34 through resistor 123 and to ground through diode 122. The output terminal is further connected to an input terminal on amplifier 128 through resistor 124. The same input terminal is connected to the output terminal of amplifier 128 through resistor 129 and to a source of potential through resistors 127 and 125 and to ground through resistor 127 and diode 126. The output of amplifier 128 is connected to the input of amplifier 131 through resistor 130. The same input terminal is connected to the output terminal of amplifier 131 through capacitor 132 having a resistor 133 in parallel therewith. The other input terminal is connected to ground. The output terminal of amplifier 131 is connected to the lower input terminal on amplifier 108 through resistor.
Similarly, the output winding 135 on velocity transducer 26 is connected to inner meter 35 through amplifier 140, amplifier 148, amplifier 150, amplifier 160, potentiometer 72, amplifier 164, amplifier 167, demodulator 173 and 181, amplifier 189, voltage comparator 374, flip-flop 380, digital counter 203-204, resistor network 205 and amplifier 206. The output of amplifier 206 is connected to voltage comparator 374 through amplifiers 211 and 214, and the output of digital counter 203-204 is connected to the reset terminal on flip-flop 380 through nand gate 202 and amplifier 201. It may also be noted that the output of the resistor network 119 is connected to the output terminal of amplifier 102 through conductor 105 and flip-flop 104. Similarly, the output of resistor network 205 is connected to the output terminal of amplifier 189 through flip-flop 191.
Referring specifically to FIG. 6A, it may be noted that an interconnection between the two signal processing paths shows the output of amplifier 58 connected to the input of amplifier 150 through resistor 151, amplifier 152 and resistor 154. The output terminal of amplifier 152 is also shown connected to the input terminal that is connected to resistor 151. The other input terminal is connected to ground. There is also a connection existing between the output of amplifier 63 and the output of amplifier 150 through resistor 155, resistor 156 and potentiometer 157.
Referring now to FIGS. 6B, 6D, 6E and 6G, the left hand end of FIG. 6B represents the signals received from disk 27 and its adjacently disposed sources of illumination 30 and radiation responsive signal generating elements shown in the form of transistors 31, 32 and 33. The light emitting diodes D, C and R are energized from the power supply (not shown) from the negative terminal through the diodes to a ground terminal through resistor 217. The output of transistor 31 is connected to an input terminal on amplifier 220. The input terminal is connected intermediate positive and negative terminals on the power supply (not shown) through resistors 214 and 218. The other input terminal on amplifier 220 is connected to its output terminal through resistor 222 and to ground through resistor 221. The output of amplifier 220 is connected to input terminals on nand gates 227 and 228 through resistor 223. The output terminal on amplifier 220 is also connected to the voltage source through resistor 224.
The output of transistor 32 is connected to an input terminal on amplifier 235 which is in turn connected to positive and negative sources of voltage (not shown) through resistors 233 and 234, respectively. The output terminal of amplifier 235 is connected to another input terminal through resistor 237 and to ground through resistor 236. The outputof amplifier 235 is connected to inverter 240 through resistor 238 and to a source of voltage through resistor 239. The output of inverter 240 is connected to an input terminal flip-flop 226 and to the input of phase lock loop 254. Flip-flop 226 also has a clock terminal connected to an oscillator comprised of amplifiers 241 and 244. The input terminals of amplifier 241 are connected to its output terminal and the output terminal of amplifier 244 through resistor 242 and resistor 243 and capacitor 245, respectively. The output terminal on amplifier 241 is connected to an input terminal on amplifier 244, the output terminal of which is connected to the clock terminal indicated by 3 on flip-flop 226, and to the clock terminal indicated by 11 on flip-flop 225. The Q terminal on flip-flop 226 is connected to an input terminal on nand gate 228. The Q terminal on flip-flop 226 is connected to the D or drive terminal on flip-flop 225. The Q terminal on flip-flop 225 is connected to an input terminal on nand gate 227 and the Q terminal on flip-flop 225 is connected to an input terminal on nand gate 228. It should be noted that the oscillator connected to the clock terminals on flip-flop 225 operates at a substantially higher, in the order of ten times or more higher, frequency than the signals which are generated by disk 27 through its apertures 28 to transistors 31 and 32. The output of nand gate 227 is connected to input terminals on nand gates 229 and 231 and the output of nand gate 228 is connected to input terminal on nand gate 230 and an input terminal on nand gate 231. The output of nand gate 229 is connected to an input terminals on nand gate 230 and nand gate 231. The output of nand gate 230 is connected to an input terminal on nand gate 229 and to the up-down direction terminals 10 on up-down counters 273 and 272. The output of nand gate 231 is connected to count terminals 15 on binary counters 273 and 272, respectively, through nand gate 232, and to the clock terminals 1 on binary counters 118 and 203. The outputs Q4, Q3, Q2 and Q1 on up-down counter 272 are connected to inputs D4, D3, D2 and D1 on hex latches 277 and 278. Output terminals Q6 and Q5 on up-down counter 273 are connected to input terminals on exclusive or gates 275 and 274, respectively, and further to input terminals on the indicated exclusive or gates connected to the output of hex latches 277 and 278. The output of exclusive or gate 275 is connected to input terminals D4 on hex latches 277 and 278 and to an input terminal on exclusive or gate 274. The output of exclusive or gate 274 is connected to an input of exclusive or gate 276 and to terminals D6 on hex latches 277 and 278. It should also be noted that the output terminals of hex latches 277 and 278 are connected to input terminals of certain ones of the exclusive or gates appearing adjacent the right sides of hex latches 277 and 278 with the connections performed as indicated. The outputs of the exclusive or gates are connected to a pair of nor gates and thence to nand gates 280 and 279, respectively. The output of nor gate 280 is connected to an input terminal of a nand gate 289, the output of which is connected to inner indicator lamp 37 through resistor 300 having diode 301 in parallel therewith, the input terminal of amplifier 306, such input terminal also being connected to ground through capacitor 302, resistor 303 and transistor 305 through indicator 37 to a source of negative potential (not shown). The output of nand gate 279 is connected to an input terminal of nor gate 290, the output of which is connected to outer indicator 36 through resistor 308 having diode 307 in parallel therewith, the input terminal of amplifier 309, such input terminal being connected to ground through capacitor 310, resistor 311 and transistor 312.
The count terminal 9 on hex latches 277 and 228 is controlled from flip- flops 287 and 335, respectively. These are in turn controlled from a signal derived from the zero crossing of the velocity signal appearing in the inner and outer channels which correspond to the positional information that is to be processed for the inner and outer channels. Flip-flop 287 is connected to the inner channel at the output of amplifier 167 through conductor 170 connected to an input terminal of amplifier 256, the output of which is connected to the C terminal of flip-flop 287 through resistor 284. The C terminal is also shown connected to a source of voltage through resistor 275. The output of amplifier 256 is connected to an input terminal through resistor 283 and to ground through resistor 282.
Similarly, flip-flop 335 is connected to the output of amplifier 79 through conductor 83, resistor 330 connected to an input terminal on amplifier 229 and resistor 333. The C terminal on flip-flop 335 is also connected to a source of potential through resistor 334 and the output terminal on amplifier 229 is connected to an input terminal through resistor 332 and to ground through resistor 331.
Referring to the center middle portion of FIG. 6B, an oscillator comprised of a multivibrator 250 is shown having resistors 252 and 253 intermediate its terminals 2 and 3 and a capacitor, 254, connected between terminals 1 and 3 and other terminals connected to either a source of voltage or to ground. The output is applied to a phase locked loop which is shown having its output connected to ground through resistor 255 and to amplifier 260 through resistor 256 and 257. That the input terminal on amplifier 260 is also connected to ground through capacitor 259. The junction between resistors 256 and 257 is connected to a further input terminal on amplifier 260 through a capacitor 258 and that input terminal and output terminal are shown interconnected. The output of amplifier 260 is connected to the input of amplifier 263 through resistor 261 and to a source of negative potential through resistor 262. The other output terminal of amplifier 263 is shown connected to ground through resistor 264 and to its output terminal through resistor 265. A further resistor 266 is shown connecting the output of amplifier 263 to one of the terminals on single pole double throw switch 268. The same terminal on switch 268 is also connected to a source of positive potential through resistor 267. In the run position of switch 268, the output of amplifier 263 is applied to input terminal CA of binary counter 270.
At the bottom of FIG. 6B of the drawings, transistor 33 is shown having its output connected to an input terminal on amplifier 322 and to positive and negative sources of voltage through resistors 320 and 321, respectively. Another input terminal on amplifier 322 is connected to ground through resistor 323 and to the output terminal through resistor 324. The output of amplifier 322 is connected to the EA terminal on binary counter 270. The right end of resistor 325 is connected to a positive source of potential through resistor 326 and to ground through capacitor 327.
The Q5 and Q1 outputs of binary counters 270 and 271, respectively, are connected to the input terminals of nand gate 328. One of the input terminals (6) of nand gate 328 is connected to the 5 and 9 terminals of flip- flops 335 and 287, respectively, and to the clock terminals 3 and 11 on flip- flops 113 and 148, respectively. The output terminal of nand gate 328 is connected to an input terminal on nand gate 349 through a capacitor 339, the other input of nand gate 349 is connected to the output of nand gate 293 through resistor 348 and to an input terminal on nand gate 294. Nand gate 293 has one input terminal connected to the top of resistor 296 and the other input terminal connected to the output of nand gate 294. The other input terminal of nand gate 294 is connected to the lower end of resistor 295 and the junction between resistors 295 and 296 is connected to a source of potential (not shown) as may be seen on the start-stop switch at the bottom of FIG. 6G of the drawing, one or the other end of resistors 296 and 295 may be connected to ground. The output of nand gate 349 is connected to the reset terminal on flip-flop 352 through resistor 350. The Q output terminal on flip-flip 352 is connected to input terminals 5 and 2 on nor gates 289 and 270 and to amplifier 353. The output of amplifier 353 is connected to the forward winding on motor 11 through resistor 356 having capacitor 355 and resistor 357 in parallel therewith through transistor 358 connected to a source of potential (not shown) to the winding. The output of amplifier 353 is also connected to the count terminal on flip-flop 357. Flip-flop 357 is shown with its reset terminal at the lower bottom connected through a resistor 172 to the output of an inverter 171 and to the output of nor gate 170. The Q terminal on flip-flop 357 is connected to the reverse motor winding 365 through amplifier 360, having its output connected to the Q terminal on flip-flop 357 and to transistor 364 through resistor 363 having capacitor 361 and 362 in parallel therewith and having an emitter terminal connected to a source of potential (not shown).
A pair of NAND gates 291 and 292 are shown having their output terminals interconnected to the respective input terminals and the other input terminals connected across resistors 297 and 298 which are connected to the start-stop switch at the bottom of FIG. 6G to be alternately connected to ground. The mid-points of resistors 297 and 298 are connected to a source of potential (not shown), the output of NAND gate 292 is connected to the count terminal on flip-flop 352 and the lower terminal on nor gate 170 and the output terminal on nand gate 291 is connected to the reset terminals on hex counters 277 and 278.
Referring to the bottom of FIG. 6E, an exclusive or gate 340 is shown having one input terminal connected to ground and the other input terminal connected to ground through capacitor 342 and to a source of potential (not shown) through resistor 341. The output of exclusive or gate 340 is connected to the base electrode of transistor 346 through resistor 243 and to the emitter and a source of positive potential (not shown) through resistor 344. The collector of transistor 346 is connected to ground through resistor 345 and, through diode 288, to the reset terminals on flip- flops 287 and 335, the reset terminals are A and b on binary counters 270 and 271 and to the reset terminals on binary counters 118, 203 and 204; and to the reset terminals on flip- flops 352 and 357 through diodes 351 and 173, respectively; and to the reset terminals on flip- flops 113 and 148 through diodes 115 and 146, respectively. The following is a table of values of components used in the fabrication of the illustrative embodiment:
______________________________________                                    
Reference                                                                 
         Value                                                            
Character                                                                 
         (Part No.)        Manufacturer                                   
______________________________________                                    
48       130K resistor                                                    
49       20k resistor                                                     
50       100 ohm resistor                                                 
51       .12 microfarad                                                   
         capacitor                                                        
52       dual op amp       Motorola                                       
         MC1458CP-1                                                       
53       18.2K ohm resistor                                               
54       10K ohm resistor                                                 
55       130K ohm resistor                                                
56       .12 microfarad                                                   
         capacitor                                                        
57       20K ohm resistor                                                 
58       Type MC1458CP-1                                                  
         dual op amp       Motorola                                       
59       200K ohm resistor                                                
60       1MEG. ohm potentiometer                                          
62       30K ohm resistor                                                 
63       Type MC1741CP-1                                                  
         op amp            Motorola                                       
64       5.11K ohm resistor                                               
65       61.9K ohm resistor                                               
66       .27 microfarad                                                   
         capacitor                                                        
67       124K ohm resistor                                                
68       Type MC1458CP-1                                                  
         dual op amp       Motorola                                       
69       453K ohm resistor                                                
70       .018              microfarad                                     
         capacitor                                                        
73       124K ohm resistor                                                
74       Type MC1458CP-1                                                  
         dual op amp       Motorola                                       
75       .018 microfarad                                                  
         capacitor                                                        
76       453K ohm resistor                                                
77       .27 microfarad                                                   
         capacitor                                                        
78       124K ohm resistor                                                
79       Type MC1741CP-1                                                  
         op amp            Motorola                                       
80       124K ohm resistor                                                
81       6.9K ohm resistor                                                
82       15 microfarad                                                    
         capacitor                                                        
84       20K ohm resistor                                                 
85       Type LM308N op amp                                               
                           National                                       
                           Semiconductor                                  
86       20 microfarad                                                    
         capacitor                                                        
87       10K ohm resistor                                                 
90       20K ohm resistor                                                 
92       20K ohm resistor                                                 
93       10K ohm resistor                                                 
94       Type LM310N       National                                       
         voltage follower  Semiconductor                                  
95       6.81K ohm resistor                                               
96       20 picofarad                                                     
         capacitor                                                        
97       22.1K ohm resistor                                               
99       18.2K ohm resistor                                               
100      6.8 microfarad                                                   
         capacitor                                                        
101      18.2K ohm resistor                                               
102      Type LM310N       National                                       
         voltage follower  Semiconductor                                  
103      3.3 microfarad                                                   
         capacitor                                                        
104      Type CD4016AE     RCA                                            
         analog switch                                                    
106      4.7K capacitor                                                   
108      Type LM339N       National                                       
         quad comparator   Semiconductor                                  
109      270K ohm resistor                                                
110      100 ohm resistor                                                 
111      10K ohm resistor                                                 
112      10K ohm resistor                                                 
113      Type CD4013AE     RCA                                            
         flip-flop                                                        
116      Type CD4011AE     RCA                                            
         nand gate                                                        
117      Type CD4068BE     RCA                                            
         nand gate                                                        
118      Type CD4520BE     RCA                                            
         binary counter                                                   
119      Type 316LO8104    Alan Bradley                                   
         resistor network                                                 
120      .001 micro-farad capacitor                                       
121      Type LM310N       National                                       
         voltage follower  Semiconductor                                  
123      6.04K ohm resistor                                               
124      10K ohm resistor                                                 
125      1.1K ohm resistor                                                
127      124K ohm resistor                                                
128      Type MC1458CP-1   Motorola                                       
         dual op amp                                                      
129      10K ohm resistor                                                 
130      10K ohm resistor                                                 
131      Type MC1458CP-1   Motorola                                       
         dual op amp                                                      
132 100 picrofarad                                                        
         capacitor                                                        
133      100K resistor                                                    
136      130K resistor                                                    
137      20K ohm resistor                                                 
138      100 ohm resistor                                                 
139      .12 microfarad                                                   
         capacitor                                                        
140      Type MC1458CP-1   Motorola                                       
         dual op amp                                                      
141      18.2K ohm resistor                                               
142      10K ohm resistor                                                 
143      .12 microfarad                                                   
         capacitor                                                        
144      130K ohm resistor                                                
145      20K ohm resistor                                                 
146      316K ohm resistor                                                
147      1MEG. ohm potentiometer                                          
148      Type LM308N       National                                       
         op amp            Semiconductor                                  
149      124K ohm resistor                                                
150      Type MC1458CP-1   Motorola                                       
         dual op amp                                                      
151      100K ohm resistor                                                
152      (see 150)                                                        
153      100K ohm resistor                                                
154      124K ohm resistor                                                
155      124K ohm resistor                                                
156      61.9 ohm resistor                                                
157      200K ohm resistor                                                
158      .27 microfarad                                                   
         capacitor                                                        
159      124K ohm resistor                                                
160      Type MC1458CP-1   Motorola                                       
         dual op amp                                                      
161      124K ohm resistor                                                
162      .018 microfarad                                                  
         capacitor                                                        
163      453K ohm capacitor                                               
164      (see 160)                                                        
165      .27 microfarad                                                   
         capacitor                                                        
166      124K ohm resistor                                                
167      Type MC1741CP-1   Motorola                                       
         op amp                                                           
168      61.9K ohm resistor                                               
169      124K ohm resistor                                                
171      15 microfarad                                                    
         capacitor                                                        
172      20K ohm resistor                                                 
173      Type LM308N       National                                       
         op amp            Semiconductor                                  
174      10K ohm resistor                                                 
175      20 picofarad                                                     
         capacitor                                                        
178      20K ohm resistor                                                 
180      10K ohm resistor                                                 
181      Type LM308N       National                                       
         op amp            Semiconductor                                  
182      20 picofarad                                                     
         capacitor                                                        
183      6.81K ohm resistor                                               
184      22.1K ohm resistor                                               
186      18.2 ohm resistor                                                
187      18.2 ohm resistor                                                
188      6.8 microfarad                                                   
         capacitor                                                        
189      Type LM310N       National                                       
         voltage follower  Semiconductor                                  
190      3,3 microfarad                                                   
         capacitor                                                        
191      Type CD4016AE     RCA                                            
         analog switch                                                    
192      Type LM3391       National                                       
         quad comparator   Semiconductor                                  
193      270K ohm resistor                                                
194      10K ohm resistor                                                 
195      100 ohm resistor                                                 
198      Type CD4013AE     RCA                                            
         flip-flop                                                        
199      10K ohm resistor                                                 
200      48.7K ohm resistor                                               
201      Type CD4011AE     RCA                                            
         nand gate                                                        
202      Type CD4068BE     RCA                                            
         nand gate                                                        
203      Type CD4520BE     RCA                                            
         binary counter                                                   
204      (see 203)                                                        
205      Type 316L08104    Alan Bradley                                   
         resistor network                                                 
206      Type LM310N       National                                       
         voltage follower  Semiconductor                                  
207      .001 microfarad                                                  
         capacitor                                                        
209      6.04K ohm resistor                                               
210      10K ohm resistor                                                 
211      Type MC1458CP-1;  Motorola                                       
         dual op amp                                                      
212      10K ohm resistor                                                 
213      10K ohm resistor                                                 
214      Type MC1458CP-1   Motorola                                       
         dual op amp                                                      
215      10K ohm resistor                                                 
216      1000 picofarad                                                   
         capacitor                                                        
217      150 ohm resistor                                                 
218      150K ohm resistor                                                
219      9K ohm resistor                                                  
220      Type LM339N       National                                       
         quad comparator   Semiconductor                                  
221      15K ohm resistor                                                 
222      270K ohm resistor                                                
223      10K ohm resistor                                                 
224      10K ohm resistor                                                 
225      Type CD4013AE     RCA                                            
         flip-flop                                                        
226      (see 225)                                                        
227      Type CD4023AE     RCA                                            
         nand gate                                                        
228      (see 227)                                                        
229      Type CD4011AE     RCA                                            
         nand gate                                                        
230      (see 229)                                                        
231      (see 216)                                                        
232      (see 219)                                                        
233      91K ohm resistor                                                 
234      150K ohm resistor                                                
235      Type LM339N       National                                       
         quad comparator   Semiconductor                                  
236      15K ohm resistor                                                 
237      270K ohm resistor                                                
238      10K ohm resistor                                                 
239      10K ohm resistor                                                 
240      Type CD4011AE     RCA                                            
         nand gate                                                        
241      Type MC14572CP    Motorola                                       
         multifunction I.C.                                               
242      200K ohm resistor                                                
243      20K ohm resistor                                                 
244      (see 241)                                                        
245      680 picofarad                                                    
         capacitor                                                        
250      Type CD4047AE     RCA                                            
         astable multivibrator                                            
251      .018 microfarad                                                  
         capacitor                                                        
252      18.2K ohm resistor                                               
253      5K ohm resistor                                                  
254      Type CD4046AE     RCA                                            
         phase lock loop                                                  
255      20K ohm resistor                                                 
256      220K ohm resistor                                                
257      220K ohm resistor                                                
258      .1 microfarad                                                    
         capacitor                                                        
259      .05               microfarad                                     
         capacitor                                                        
260      Type MC1741CP-1   Motorola                                       
         op amp                                                           
261      10K ohm resistor                                                 
262      20K ohm resistor                                                 
263      Type LM339AN      National                                       
         quad comparator   Semiconductor                                  
264      1K ohm resistor                                                  
265      270K ohm resistor                                                
266      10K ohm resistor                                                 
270      Type CD4520BE     RCA                                            
         binary counter                                                   
271      (see 270)                                                        
272      Type CD4516BE     RCA                                            
         up-down counter                                                  
273      (see 272)                                                        
274      Type CD4030AE     RCA                                            
         exclusive or gate                                                
275      (see 274)                                                        
276      (see 274)                                                        
277      Type MM74C174N    National                                       
         hex latch         Semiconductor                                  
278      (see 277)                                                        
279      Type CD4011AE     RCA                                            
         nand gate                                                        
280      (see 279)                                                        
281      22 ohm resistor                                                  
282      200 ohm resistor                                                 
283      270K ohm resistor                                                
284      10K ohm resistor                                                 
285      10K ohm resistor                                                 
286      Type LM339AN      National                                       
         quad comparator   Semiconductor                                  
289      Type CD4001AE     RCA                                            
         Nor gate                                                         
290      (see 289)                                                        
291, 292,                                                                 
         Type CD4011AE                                                    
293, 294 nand gate                                                        
295, 296,                                                                 
         4.7K ohm resistor                                                
297, 298                                                                  
300      82K ohm resistor                                                 
302      2.2 microfarad                                                   
         capacitor                                                        
303      1K ohm resistor                                                  
304      10K ohm resistor                                                 
305      Type 2N4403                                                      
         transistor                                                       
306      Type CD4049AE     RCA                                            
         inverted buffer                                                  
307      82K ohm resistor                                                 
309      (see 306)                                                        
310      2.2 microfarad                                                   
         capacitor                                                        
311      1K ohm resistor                                                  
312      Type 2N4403                                                      
         transistor                                                       
313      10K ohm resistor                                                 
320      91K ohm resistor                                                 
321      150K ohm resistor                                                
322      Type LM339AN      National                                       
         quad comparator   Semiconductor                                  
323      15K ohm resistor                                                 
324      270K ohm resistor                                                
325      10K ohm resistor                                                 
326      10K ohm resistor                                                 
327      100 picofarad                                                    
         capacitor                                                        
328      Type CD4011AE     RCA                                            
         nand gate                                                        
329      Type LM339AN      National                                       
         quad comparator   Semiconductor                                  
330      22 ohm resistor                                                  
331      200 ohm resistor                                                 
332      270K resistor                                                    
333      10K resistor                                                     
334      10K resistor                                                     
335      Type CD4013AE     RCA                                            
         flip-flop                                                        
336      10K ohm resistor                                                 
339      .1 microfarad                                                    
         capacitor                                                        
340      Type CD4030AE     RCA                                            
         exclusive or gate                                                
341      270K resistor                                                    
342      1 microfarad                                                     
         capacitor                                                        
343      4.7K ohm resistor                                                
344      10K ohm resistor                                                 
345      10K ohm resistor                                                 
346      2N4403                                                           
         transistor                                                       
347      100K ohm resistor                                                
348      20K ohm resistor                                                 
349      Type CD4011AE     RCA                                            
         nand gate                                                        
350      10K ohm resistor                                                 
352      Type CD4013AE     RCA                                            
         flip-flop                                                        
353      Type MC14572CP    Motorola                                       
         multifunction I.C.                                               
354      (see 352)                                                        
355      .05 microfarad                                                   
         capacitor                                                        
356      1K ohm resistor                                                  
357      10K ohm resistor                                                 
358      Type 2N4403                                                      
         transistor                                                       
360      (see 353)                                                        
361      .05 microfarad                                                   
         capacitor                                                        
362      10K ohm resistor                                                 
363      1K ohm resistor                                                  
364      Type 2N4403                                                      
         transistor                                                       
370, 371 (see 352)                                                        
372      10K ohm resistor                                                 
373      124K ohm resistor                                                
374      Type LM339N quad                                                 
         comparator                                                       
375      270K ohm resistor                                                
376      10K ohm resistor                                                 
377      100 ohm resistor                                                 
378      100 ohm diode                                                    
379      100 ohm diode                                                    
380      Type CD4013AE     RCA                                            
         flip-flop                                                        
______________________________________
OPERATION
In considering the operation of our invention, it is assumed that a wheel-tire system has been suitably mounted on axle 12 for rotation therewith with its inner and outer planes of rotation 22 and 21 disposed so that plane 22 is in the plane of rotation of the axle engaging and supporting portion at the right end of tubular projection 15 on bearing 14, as illustrated in FIG. 2. The rim width is determined and potentiometer 61, having previously been calibrated in units of rim width, is adjusted as well as rim diameter potentiometers 71 and 72, which likewise have been calibrated in terms of units of diameter for the wheel, are likewise adjusted so that the computations performed relative to the magnitudes of the forces of unbalance may be directly read on meters 34 and 35 in units of weight of material to be added at predetermined angular positions on the rim of the wheel-tire system.
It will be assumed that the start-stop switches are initially in the position shown and that the power supply (not shown) is energized. At this time, a pulse supplied to transistor 346 from exclusive or gate 340 (FIG. 6E) provides a reset pulse to reset terminals on motor drive flip-flops 352 and 357 (FIG. 6G), each providing an output which results in the continuing de-energization of motor forward and reverse windings 354 and 365. A further pulse is applied to the reset terminals of flip- flops 113 and 148 effectively disconnecting meters 34 and 35. The same output is connected to the reset terminals on binary counters 270 and 271 and to the reset terminals on binary counters 118 and 203-204. Oscillator 250 is energized and operative to oscillate at a frequency related to the desired velocity of revolution of shaft 12, as determined by the number of apertures 28 in disk 27, its output is connected to phase lock loop 254 which results in no output at switch 268. Further, the high frequency, in the magnitude of ten times the frequency of oscillator 250, oscillator is energized to continuously clock flip-flops 225 and 226 (FIG. 6B). Further, the output of flip-flop 352 on FI. 6G is of a polarity as to inhibit the operation of nor gates 289 and 290 so that no output therefrom will be applied to inner and outer indicators 37 and 36 (FIG. 6G). There are no signals applied to any of the input channels shown at the left end of FIG. 6A and 6B for the magnitude-force and phase and frequency sources of signal.
At this stage, the apparatus is in readiness for the determination of the amount of unbalance and the necessary action to be taken by the operator as far as adding weights at predetermined locations in the two planes of rotation of wheel-tire system 20-23; namely, at the rim of the wheel 20 at the angular positions to be determined.
The operator initiates the operation by momentarily reversing the contacts on the start-stop button shown at the lower left hand end of FIGS. 6G. This results in the application of a pulse to the C terminal of flip-flop 352 from nand gate 292 which in turn results in a Q output which, when conveyed through inverter 353 to transistor 358 results in the energization of motor forward drive winding 354. Simultaneously, an inhibit pulse is transmitted from the Q terminal of flip-flop 352 to NOR gates 289 and 290 for inhibiting the application of any output to inner and outer indicators 37 and 36. Simultaneously, an output from nand gate 291 to the reset terminals on hex counters 277 and 278 places them in condition for registering and storing information concerning the angular positions of shaft 12. At the same time, the reversal of the state of the multivibrator comprised of nand gates 293 and 294 in the lower left hand corner of FIG. 6G results in a removal of the reset signal from nand gate 349 to reset terminal 10 on flip-flop 352. The forward winding of motor 10 is thus energized and motor 10 is operative to initiate and accelerate the rotational speed of shaft 12. As the shaft rotates, force signals proportional to the velocity of displacement of shaft 12 in the horizontal plane 16 are generated by transducers 25 and 26, which are in turn applied to the windings 47 and 135 on the inner and outer channels (extendings from FIGS. 6A through FIG. 6C to FIG. 6F), which will result in an indication on meters 35 and 34, respectively, of the amount of weights will be needed to compensate for the unbalance in the wheel-tire system. Simultaneously, signals will be provided to phototransistors 31, 32 and 33, corresponding to the angular position and rotational velocity of shaft 12. At this time, flip- flops 113 and 148 and nor gates 289 and 290 inhibit the transmittal of signals corresponding to weight and angle to the operator indicators comprising meters 34, 35, and lights 37, 36. As motor 11 increases the rotational velocity of shaft 12 to a speed which corresponds to that determined by oscillator 250 (middle portion of FIG. 6B) phase lock loop 259 will become operative to transmit the oscillator signal as a clock to the timing circuit comprised of binary counters 270 and 271 which is enabled once a revolution by the velocity of rpm signal supplied from photoelectric transistor 33, such signal is also supplied to up-down counters 273 and 272, to reset the counters at the beginning of every revolution of operation of shaft 12. The initiation of the counting function of binary counters 270 and 271 (left end of drawings FIG. 6E) results in a signal applied to nand gate 328 from the Q terminal 11 on binary counter 271 and to the drive terminals of flip-flops 287 and 335 (middle portion, FIG. 6E) as well as to the C2 terminals on flip-flops 113 and 148 (middle left portion of FIG. 6F). During the time interval determined by the number of counts necessary to cause the Q3 and Q1 outputs on binary counters 270 and 271 to appear in time coincidence, binary counter 270 continues to receive an enabling signal once every revolution so that it may accept clock pulses from oscillator 250 to continue its counting operations and up-down counters 273 and 272 are reset at the beginning of every revolution by the signals determined from photoelectric transistor 33 in response to aperture 29 in disk 27. Simultaneously, flip-flops 225 and 226, and nand gates 227 and 228 and 231 and 232 will be operative to provide the counting pulse train to counters 273 and 272, the outputs of which are combined to form a code which is applied to the inputs of hex latches 277 and 278 to thereby control the respective output terminals indicated by Q1, Q6. The output of the hex latches which continuously step up and down in accordance with the signals provided from up-down counters 273 and 272, and which continue to change as shaft 15 rotates, are connected, in each case, to a plurality of logic elements shown in the form of exclusive or gates, nor gates, and each culminating in a hand gate 280 and 279, respectively, the output of which may be used to activate inner and outer indicators 37 and 36, respectively. It should be noted at this point that indicators 37 and 36 are each energized through a fast-on, slow-off network including resistor 300, diode 301, capacitor 302 and inverter 306, in the case of the "inner" channel.
Further, during the same time interval, the signals applied to the outer and inner channels appearing at FIG. 6A, FIG. 6E, and FIG. 6F, first proceed, in the case of both channels, through a zero phase shift signal processing portion of the channels up to capacitors 92 and 171, respectively, at which point they are still in the form of alternating potentials which have a magnitude corresponding to the degree of velocity of unbalance for any given angular position of shaft 12 as an instantaneous signal. It may be noted that the inner channel's signal is modified by the introduction of selected portions of the outer channel signal through amplifier 152 and the interconnection between the output of amplifier 63 and amplifier 150.
After the signals have been thus processed, they are each demodulated and filtered to provide a dc level corresponding to the magnitude of the maximum unbalance of the wheel-tire system. These signals are compared in comparators 108 and 142, the output of which is applied to binary counters 118 and 203-204, respectively. The counters continue to operate according to the frequency of the clock signal applied from the output of nand gate 232 (corresponding to the angular outer and inner meters 34 and 35 will reflect the average level of the force unbalance signals as determined by the displacement of bearings 13 and 14 from their normal positions).
It should be noted that the operation of hex latches 277 and 278 and the associated logic connected to their respective outputs and the logic associated with the outputs of up-down counters 273 and 272 is such that by using the connections indicated (only some of which are shown as complete conductors) a 90° phase shift is computed into the operation of the counters for the logic associated with the hex latches so that when a real time positional signal is present in the hex latches, the logic consisting of the exclusive or and nor gates connected between hex latches 277 and 278 and nand gates 280 and 279, respectively, will respond to a particular count with a 90° shift. This is occasioned by the operations performed in the integration of the velocity of displacement signal supplied to the two channels of FIG. 6A, 6C and 6F. The hex latches will operate continuously to store the signals applied to them until the first zero crossing of the signals appearing at amplifiers 79 and 167 at which time flip- flops 287 and 335 are toggled by zero crossing detectors 256 and 229 to "latch" hex latches 277 or 278 to store the signal appearing therein at that instant. This signal will be available for the illumination of indicators 37 or 36 in subsequent phases of operation of the machine.
When coincidence is reached for the outputs of binary counters 270 and 272 for the indicated terminals Q3 and Q1, respectively, nand gate 328 transmits a signal to nand gate 349 which resets flip-flop 352 to de-energize motor forward winding 354, removes the inhibit signal from nor gates 289 and 290 and supplies a pulse to toggle flip-flop 357 to energize motor reverse winding 365. At this point in the cycle of operation, flip- flops 113 and 148 have been toggled by the operation of comparators 108 and 142 in driving binary counters 118 and 203-204 to a condition which supplies an output voltage through digital to analog converters 119 and 205 so that the energization of meters 34 and 35, calibrated in convenient units, will indicate the correct total of weight to be supplied to the inner and outer planes of rotation of the wheel-tire system.
The energization of reverse winding 365 serves to provide a rapid braking of motor 11 and when a signal that is derived from the positional information derived from apertures 28 on disk 27, appears at the output of nand gate 229 and to nor gate 170 to the reset terminal on flip-flop 357 to thereby de-energize motor reverse winding 365 and the system is at rest.
At this time, the operator will rotate the wheel-tire system on shaft 12 until one or the other of the indicator lamps 36 or 37 is energized to indicate to the operator that he should apply a specific weight of material, such as lead balance weights, to the rim of the wheel-tire system in the indicated plane, inner plane 22 or outer plane 21. For convenience, the indicator lamp may be operative when the portion of the rim corresponding to the angular position for application of the weight is disposed vertically above the axis of rotation of shaft 12 and may take the form of a pointer or other convenient indicia that may be stationarily mounted on the base upon which the bearings and motor for the system are disposed.
When it is desired to perform another balancing act, another wheel-tire system is again disposed on the end of shaft 12 and the momentary contact start-stop switch is moved to its active position so that the movable contacts are disposed in the opposite relationship with their indicated contacts on the lower left portion of FIG. 6G to again toggle the multivibrators comprised of nand gates 291 and 292 and 293 and 294. This supplies a reset signal from terminal three on nand gate 291 to the reset terminals on hex latches 277 and 278, toggles flip-flop 352 to thereby energize motor forward winding 354 and provides the inhibit signal applied to terminals 2 and 5 on nor gates 290 and 289. The same signal is also applied to the reset terminals on flip- flops 287 and 335 through resistor 336 (FIG. 6E), to reset terminals 7 and 15 on binary counters 270 and 271 and to the reset terminals on binary counters 118 and 203-204 and the previously described operation ensues. The motor rapidly brings the wheel and tire system up to the predetermined speed and maintains the speed for sufficient time to enable the measurement functions to be completed (this need only be a few revolutions in actual practice), and then brings the motor to a rapid stop to allow the operator to complete the balancing operation by the application of weights at the appropriate locations in the amount indicated.
One of the features of our invention is concerned with the provision of a means for measuring angular position and direction of rotation with the utilization of a plurality of apertures spaced at angular positions chosen to provide the revolution necessary for effecting a satisfactory balancing of the wheel-tire system. In one embodiment, 64 apertures 28 were disposed on a common radius around the periphery of disk 27. A pair of sources of radiation 30, which may take the form of light emitting diodes, were disposed at the same angular spacing and a pair of photoelectric transistors 31 and 32 were disposed with the center axis of transistor 31 and the center axis of transistor 32 angularly spaced a distance somewhat less than the center axes of the equally spaced apertures 28. This, though the logic associated with transistors 31 and 32, provides an output from nand gate 229 whenever the disk is running in a reverse direction and an output from nand gate 232 whenever the disk is running in a forward direction, the total number of pulses being equal to the total number of apertures for the angular revolution required. In the present system, the clock in the forward direction provided for up-down counters 273 and 272 and for binary counters 118 and 203-204 consists of 64 pulses per revolution at a constant frequency when the motor is driving shaft 11 at the desired speed.
The test functions associated with switch 169 on the lower right hand corner of FIG. 6B and the switch and functions associated with analogue switch 104 and 191 at the top of FIG. 6C are not essential to the operation of our invention and therefore the description and operation of same are not included.

Claims (30)

We claim:
1. Electronic wheel balancing apparatus comprising in combination:
(a) a shaft for rotatably mounting a wheel and tire;
(b) reversible motor means driveably connected to said shaft;
(c) control means for energizing said motor from a source of energy;
(d) first and second bearing means rotatably journaling said shaft, said bearing means having mounting means permitting motion thereof in parallel planes,
(e) first and second sources of signal connected to said first and second bearing means, said first and second sources of signal being indicative of the velocity of motion of the respective bearing means;
(f) third and fourth sources of signal, said third source of signal being indicative of the angular position of said shaft and the direction of rotation of said shaft, and said fourth source of signal being indicative of the rotational velocity of said shaft;
(g) signal responsive means connected to said first and second signals to indicate the magnitude of an imbalance in each of said planes and connected to said third signal to indicate the angular location of an imbalance in each of said planes;
(h) means connecting said sources of signal to said control means whereby said motor means is energized to attain a predetermined rotational velocity, the first and second signals are displayed on said signal responsive means to indicate the magnitude of imbalance in each of said planes, the third signal is displayed on said signal responsive means for indicating the angular location of the imbalance in each of said planes;
(i) means to energize said motor means in a reverse direction to thereby tend to stop said shaft; and,
(j) means to de-energize said motor when the positional source of signal reverses direction allowing said shaft to remain at rest.
2. Electronic wheel balancing apparatus of claim 1 further comprising means to inhibit said signal responsive means from accepting the first, second, third and fourth signals until said shaft attains said predetermined rotational velocity.
3. Electronic wheel balancing apparatus of claim 1 wherein said signal responsive means for each plane comprises a digital means indicating the magnitude of weight to be added to said tire and wheel and indicating the angular position of said tire and wheel for adding the weight.
4. Electronic wheel balancing apparatus of claim 1 wherein said signal responsive means for each plane comprises an indicating meter and an indicating lamp whereby said meter indicates the magnitude of weight to be added to said tire and wheel and said lamp indicates the correct angular position for adding the weight.
5. Electronic wheel balancing apparatus of claim 1 wherein said signal responsive means comprises an indicating meter and an indicating lamp for an inner plane and outer plane of said tire and wheel whereby said meter indicates the magnitude of weight to be added and said lamp indicates the correct angular position for adding the weight to the inner and outer plane of said tire.
6. Electronic wheel balancing apparatus of claim 1 wherein said signal responsive means to indicate the magnitude of weight to each plane of said tire and wheel further comprises a meter for each plane, a digital to analog converter connected to said meter, a binary counter to supply a voltage to said digital to analog converter, a flip-flop to drive said binary counter, a comparator to drive said flip-flop, and means to process said first and second signals whereby said first and second sources of signal are processed prior to being compared for each plane.
7. Electronic wheel balancing apparatus of claim 6 further comprising amplifier means and demodulating means for each source of signal connected between said source of signal and said comparator whereby said sources of signal are amplified and demodulated to provide a filtered direct current level corresponding to the magnitude of imbalance of the tire and wheel to said comparator.
8. Electronic wheel balancing apparatus of claim 1 wherein said first and second sources of signal comprise a first and second velocity detecting transducer whereby said transducers convert displacement motion in said plane of said first and second bearings into electrical signals proportional to said velocity of motion.
9. Electronic wheel balancing apparatus of claim 1 wherein said third source of signal comprises a disk, a plurality of equally spaced apart apertures disposed on said disk, and means to generate said third source of signal.
10. Electronic wheel balancing apparatus of claim 9 wherein said plurality of equally spaced apart apertures comprises 64 apertures.
11. Electronic wheel balancing apparatus of claim 9 wherein said third source signal generating means comprises two light sources on one side of said disk and two light receivers on the other side of said disk.
12. Electronic wheel balancing apparatus of claim 1 wherein said reverse motor energization means further comprises means to de-energize a motor forward winding and means to energize a motor reverse winding to dynamically brake said motor.
13. Electronic wheel balancing apparatus of claim 12 wherein said means to energize said reverse motor reverse winding and means to de-energize said motor comprises a flip-flop.
14. Electronic wheel balancing apparatus of claim 1 wherein said signal responsive means to indicate the angular position of the weight to be added to the inner and outer planes of said tire and wheel further comprises an indicator for each plane, a current responsive switch connected to said indicator, a fast-slow network connected to said switch, a first logic means connected to said network, a hex latch connected to said first logic means, a up-down counter connected to said hex latch, second logic means connected to said hex latch, a flip-flop connected to said second logic means, and means connecting said third source of signal to said flip-flops to indicate the angular position for said weights.
15. Electronic wheel balancing apparatus of claim 14 further comprising an oscillator, a phase locked loop transmitting a signal from said oscillator to binary counters and also to said up-down counter for each plane, said flip-flops being driven by said binary counters whereby said binary counter continues to receive said fourth signal once every revolution whereupon said binary and up-down counters are reset at the beginning of every revolution from said fourth signal.
16. Electronic wheel balancing apparatus of claim 1 wherein said fourth source of signal comprises a disk, a single aperture disposed on said disk, and means to generate said fourth source of signal.
17. Electronic wheel balancing apparatus of claim 16 wherein said fourth source signal generating means comprises a light source on one side of said disk and a light receiver on the other side of said disk.
18. Electronic wheel balancing apparatus of claim 1 wherein said third and fourth sources of signal comprise a disk, a plurality of equally spaced apertures disposed on a common radius of said disk, a single aperture disposed on a different radius, means to generate said third source of signal from said plurality of apertures, and means to generate said fourth source of signal from said single aperture.
19. Electronic wheel balancing apparatus of claim 18 wherein said plurality of equally spaced apart apertures comprises 64 apertures.
20. Electronic wheel balancing apparatus of claim 18 wherein said third source of signal generating means comprises two light sources on one side of said disk and two light receivers on the other side of said disk and said fourth source of signal generating means comprises a light source on one side of said disk and a light receiver on the other side of said disk.
21. Electronic wheel balancing apparatus comprising in combination;
(a) a shaft for rotatably mounting a wheel and tire;
(b) means to energize and driveably rotatate a motor connected to said shaft in a forward direction;
(c) first and second bearing means for rotatably journaling said shaft, mounting means permitting motion in one plane of each of said bearing means where said plane is parallel to the axis of rotation of said shaft, transducer means to generate a first and second signal indicative of the velocity of motion of the respective bearing means parallel to an inner and outer plane of said tire and wheel, means to process each of said signals comprising first amplifier means, means to adjust for rim width and rim diameter of said wheel demodulator means, second amplifier means, comparator means, flip-flop means, binary means, resistor network means, third amplifier means, and a display means all of which are serially connected and further including a fourth amplifier and resistive network means interconnecting said first amplifier means of each channel to indicate the magnitude of the imbalance on the inner and outer plane of said wheel and tire when said shaft reaches a predetermined rotational velocity;
(d) a disk having a plurality of equally spaced apertures on a common radius, a first and second pulse generating means generating a third signal indicative of the angular position and direction of rotation of said shaft spaced apart on said common radius comprising said first pulse generating means serially connected to a fifth amplifier means and first logic means and comprising said second pulse generating means serially connected to a sixth amplifier means, an inverter, a first flip-flop means which is clocked by an oscillator and a phase locked loop driven by an oscillator, a second logic means, counter means and binary means, first hex latch means, a third logic means and two second latch means, two second flip-flop means controlling said two hex latches and receiving signals from said second amplifier means for each of said first and second signals, a fourth and fifth logic means for each of said second hex latch means, a sixth and seventh logic means connected to said fourth and fifth logic means, a seventh amplifier means connected to each of said fourth and fifth logic means, a switching means connected to each of said seventh amplifier means, and an indicating means connected to each amplifier means to indicate the angular position of imbalance on the inner and outer plane of said wheel and tire when said shaft reaches a predetermined rotational velocity;
(e) said disk also having a single aperture on a different radius, a third pulse generating means generating a fourth signal indicative of the rotation velocity of said shaft comprising said third pulse generating means serially connected to an eighth amplifier means, said eighth amplifier connected to said binary means, a sixth logic means, a seventh logic means connected to said sixth logic means, a flip-flop and amplifier means connected to a motor means whereby said motor is dynamically energized in a reverse direction when said predetermined rotational velocity is reached and de-energized when a predetermined angular displacement in a reverse direction is detected.
22. A method for electronically balancing a tire mounted on a wheel, the steps comprising:
(a) mounting a tire and wheel on a rotatable shaft journaled in two bearings;
(b) rotating the shaft in a forward direction to a predetermined rotational velocity;
(c) deriving a first and second signal of the velocity of motion in said two bearings corresponding to an inner and outer plane of said tire and wheel;
(d) deriving a third and fourth signal of a directional angular position of said shaft and a rotational velocity of said shaft;
(e) computing the magnitude of imbalance for said inner and outer planes of said tire and wheel from said first and second signals and said angular position from said third signal when said shaft reaches said predetermined rotational velocity;
(f) displaying said magnitude of the imbalance and the angular position for said inner and outer planes of said tire and wheel; and
(g) dynamically braking said rotating shaft in a reverse direction until said shaft has reversed its direction of rotation for a predetermined angular displacement.
23. A method for electronically balancing a tire and wheel of claim 22 further comprising the steps of
(a) amplifying and demodulating said first and second signals derived from output windings of planar motion velocity detectors;
(b) comparing the outputs of said signals;
(c) averaging said comparator output to provide a digital output indication of the magnitude of the imbalance for each plane of said tire and wheel.
24. A method for electronically balancing a tire and wheel of claim 23 further comprising the step of
(a) converting the digital output to an analog output for indicating the magnitude of the imbalance for each plane of said tire and wheel.
25. A method for electronically balancing a tire of claim 22 further comprising the steps of
(a) generating light pulses as a function of the angular position of said shaft for said third signal;
(b) generating a light pulse as a function of the rotational velocity of said shaft for said fourth signal;
(c) processing said pulses of said third signal to provide indication of the angular position of said shaft for the imbalances of said inner and said outer plane of said tire and wheel; and
(d) processing said pulse of said fourth signal to provide indication of the rotational velocity of said shaft.
26. A method for electronically balancing a tire and wheel of claim 22 further comprising the step of
(a) processing said pulses from said third signal to control said dynamic braking of said shaft and the reverse rotation of said shaft over a predetermined angular displacement.
27. A method for electronically balancing a tire and wheel of claim 22 further comprising the step of
(a) inhibiting said displaying until said predetermined rotational velocity is reached.
28. A method for electronically balancing a tire and wheel of claim 22 further comprising the step of
(a) displaying the imbalance magnitude and angular position in analog form.
29. A method for electronically balancing a tire and wheel of claim 22 further comprising the step of
(a) displaying the imbalance magnitude and angular position in digital form.
30. Electronic wheel balancing apparatus comprising:
(a) a shaft for rotatably mounting a wheel and tire;
(b) control means to energize said motor from a source of energy and driveably rotate said shaft in a forward direction;
(c) first and second bearing means for rotatably journaling said shaft, mounting means permitting motion of each of said bearing means in parallel planes, each of said planes parallel to an inner and outer plane of said wheel and tire;
(d) first and second signal source means connected to said first and second bearing means, said first and second signals indicative of the velocity of motion of said first and second bearing means;
(e) third signal source means indicative of the angular position of said shaft and direction of rotation thereof;
(f) fourth signal source means indicative of the rotational velocity of said shaft;
(g) signal responsive means connected to said first and second signals to indicate on a display means the magnitude of imbalance on the inner and the outer plane of said wheel and tire when said shaft reaches a predetermined rotational velocity and connected to said third signal to indicate on a display means the angular location of imbalance on the inner and outer plane of said wheel and tire when said shaft reaches said predetermined rotational velocity; and
(h) means connected to said fourth signal to energize said motor dynamically in a reverse direction when said predetermined rotational velocity is reached and deenergize said motor when said signal responsive means connected to said third signal indicates angular rotation in a reverse direction.
US05/656,606 1976-02-09 1976-02-09 Electronic balancer for vehicle wheels Expired - Lifetime US4085619A (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
US05/656,606 US4085619A (en) 1976-02-09 1976-02-09 Electronic balancer for vehicle wheels
CA270,478A CA1101523A (en) 1976-02-09 1977-01-26 Electronic balancer for vehicle wheels
NL7701065A NL7701065A (en) 1976-02-09 1977-02-02 ELECTRONIC BALANCE DEVICE FOR VEHICLE WHEELS.
BE174642A BE851064A (en) 1976-02-09 1977-02-03 ELECTRONIC EQUIPMENT FOR BALANCING VEHICLE WHEELS
DE19772705023 DE2705023A1 (en) 1976-02-09 1977-02-07 ELECTRONIC BALANCING DEVICE FOR VEHICLE WHEELS
FR7703574A FR2340545A1 (en) 1976-02-09 1977-02-09 ELECTRONIC EQUIPMENT FOR BALANCING VEHICLE WHEELS
IT20077/77A IT1085915B (en) 1976-02-09 1977-02-09 METHOD AND ELECTRONIC APPARATUS FOR THE BALANCING OF WHEELS OF VEHICLES
JP1349877A JPS5296589A (en) 1976-02-09 1977-02-09 Device and method of electronically balancing wheel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/656,606 US4085619A (en) 1976-02-09 1976-02-09 Electronic balancer for vehicle wheels

Publications (1)

Publication Number Publication Date
US4085619A true US4085619A (en) 1978-04-25

Family

ID=24633774

Family Applications (1)

Application Number Title Priority Date Filing Date
US05/656,606 Expired - Lifetime US4085619A (en) 1976-02-09 1976-02-09 Electronic balancer for vehicle wheels

Country Status (8)

Country Link
US (1) US4085619A (en)
JP (1) JPS5296589A (en)
BE (1) BE851064A (en)
CA (1) CA1101523A (en)
DE (1) DE2705023A1 (en)
FR (1) FR2340545A1 (en)
IT (1) IT1085915B (en)
NL (1) NL7701065A (en)

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4193305A (en) * 1978-08-16 1980-03-18 Lee Hunter Vehicle wheel and tire balance testing machine
US4193304A (en) * 1977-08-19 1980-03-18 Gebr. Hofmann, G.m.b.H. & Co. KG, Maschinenfabrik Methods of and apparatus for balancing a rotor
US4250555A (en) * 1979-01-22 1981-02-10 Nortron Corporation Self-calibrating data collection system for dynamic wheel balancing machine
US4297882A (en) * 1980-04-24 1981-11-03 Autotron Equipment Corporation Wheel balancer transducer mount with improved signal to noise ratio
US4338818A (en) * 1980-07-28 1982-07-13 Fmc Corporation Method for determining error sources in a wheel balancer
GB2123159A (en) * 1982-07-06 1984-01-25 Donald B Curchod Low energy drive for dynamic balancer
US4450529A (en) * 1980-07-28 1984-05-22 Fmc Corporation Method and apparatus for determining encoder accuracy margin in a wheel balancer
US4457172A (en) * 1982-08-10 1984-07-03 Hofmann Corporation Automotive Service Equipment Electronic wheel balancer with signal conditioning
US4480472A (en) * 1982-08-10 1984-11-06 Hofmann Corporation Automotive Service Equipment Electronic wheel balancer for vehicle wheels
US4502328A (en) * 1982-08-10 1985-03-05 Hofmann Corporation Automotive Service Equipment Free spinning electronic wheel balancer
US4635481A (en) * 1982-07-06 1987-01-13 Curchod Donald B Light weight dynamic wheel balancing machine
US4958290A (en) * 1988-11-18 1990-09-18 Accu Industries, Inc. Balancer
US4980621A (en) * 1989-11-20 1990-12-25 Gebruder Hofmann Gmbh & Co. Kg Maschinenfabrik Control arrangement for controlling the power supplied to an electric motor
US5454627A (en) * 1993-07-27 1995-10-03 Bridgestone Corporation Method of correcting weight unbalance of rim-fitted tire
US5469040A (en) * 1991-07-22 1995-11-21 Hofmann Werkstatt-Technik Gmbh Operating circuit including an oscillating circuit capacitor coupled to an auxiliary winding for an apparatus that measures the unbalance of a rotary member
GB2323932A (en) * 1997-04-03 1998-10-07 Cirrus Technologies Ltd Wheel balancing apparatus using positive feedback to cause torsional instability
US5889206A (en) * 1995-10-04 1999-03-30 Muller Bem Process and device for balancing a rotating body by addition of balancing weights
US5909097A (en) * 1996-09-06 1999-06-01 Hofmann Werkstatt-Technik Gmbh Method of stopping an electric motor-driven balancing machine main shaft
US5959204A (en) * 1993-10-26 1999-09-28 Hofmann Werkstatt-Technik Gmbh Method and apparatus for holding in position a motor vehicle wheel clamped on a balancing machine measuring spindle
EP1321755A2 (en) * 2001-12-12 2003-06-25 Snap-On Equipment GmbH Method and device for balancing a vehicle wheel by rotating the wheel
US20040070388A1 (en) * 2002-10-09 2004-04-15 Chuang Thomas Hong Detecting rotational direction of a rotating article
WO2004048917A2 (en) * 2002-11-26 2004-06-10 Bombardier Transportation Gmbh Rotating equipment testing apparatus and method
US20040237647A1 (en) * 2003-06-02 2004-12-02 Youells James P. Drive location compensation system
US9146171B1 (en) * 2012-02-22 2015-09-29 Hennessy Industries, Inc. Auto calibration method and apparatus for wheel balancer equipment
US11333569B2 (en) * 2018-09-14 2022-05-17 Akron Special Machinery, Inc. Dynamic balancer with a frameless motor drive

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4191055A (en) * 1978-07-25 1980-03-04 Ransburg Corporation Dynamic imbalance determining system
IT1201517B (en) * 1979-09-05 1989-02-02 Giuseppe Donato PLANT FOR ELECTRONIC BALANCING OF WHEELS OF VEHICLES
DE4432025B4 (en) * 1994-09-08 2005-03-10 Beissbarth Gmbh balancer
DE19713075B4 (en) * 1997-03-27 2004-09-16 Snap-On Equipment Gmbh Method and device for releasably fastening a motor vehicle wheel to a main shaft of a wheel balancing machine which can be driven by a drive motor

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2886756A (en) * 1957-09-06 1959-05-12 Edward J Schaefer Plugging of single phase motors
US3774456A (en) * 1970-10-03 1973-11-27 Gkn Transmissions Ltd Apparatus for use in wheel counterbalancing

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU427621B2 (en) * 1968-09-17 1972-08-28 Repco Research Proprietary Limited Improvements in or relating to apparatus for use in balancing motor vehicle and other wheels
US3910121A (en) * 1973-08-28 1975-10-07 Nortron Corp Dynamic balancing machine

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2886756A (en) * 1957-09-06 1959-05-12 Edward J Schaefer Plugging of single phase motors
US3774456A (en) * 1970-10-03 1973-11-27 Gkn Transmissions Ltd Apparatus for use in wheel counterbalancing

Cited By (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4193304A (en) * 1977-08-19 1980-03-18 Gebr. Hofmann, G.m.b.H. & Co. KG, Maschinenfabrik Methods of and apparatus for balancing a rotor
US4193305A (en) * 1978-08-16 1980-03-18 Lee Hunter Vehicle wheel and tire balance testing machine
US4250555A (en) * 1979-01-22 1981-02-10 Nortron Corporation Self-calibrating data collection system for dynamic wheel balancing machine
US4297882A (en) * 1980-04-24 1981-11-03 Autotron Equipment Corporation Wheel balancer transducer mount with improved signal to noise ratio
US4450529A (en) * 1980-07-28 1984-05-22 Fmc Corporation Method and apparatus for determining encoder accuracy margin in a wheel balancer
US4338818A (en) * 1980-07-28 1982-07-13 Fmc Corporation Method for determining error sources in a wheel balancer
GB2123159A (en) * 1982-07-06 1984-01-25 Donald B Curchod Low energy drive for dynamic balancer
US4635481A (en) * 1982-07-06 1987-01-13 Curchod Donald B Light weight dynamic wheel balancing machine
US4457172A (en) * 1982-08-10 1984-07-03 Hofmann Corporation Automotive Service Equipment Electronic wheel balancer with signal conditioning
US4480472A (en) * 1982-08-10 1984-11-06 Hofmann Corporation Automotive Service Equipment Electronic wheel balancer for vehicle wheels
US4502328A (en) * 1982-08-10 1985-03-05 Hofmann Corporation Automotive Service Equipment Free spinning electronic wheel balancer
US4958290A (en) * 1988-11-18 1990-09-18 Accu Industries, Inc. Balancer
US4980621A (en) * 1989-11-20 1990-12-25 Gebruder Hofmann Gmbh & Co. Kg Maschinenfabrik Control arrangement for controlling the power supplied to an electric motor
US5469040A (en) * 1991-07-22 1995-11-21 Hofmann Werkstatt-Technik Gmbh Operating circuit including an oscillating circuit capacitor coupled to an auxiliary winding for an apparatus that measures the unbalance of a rotary member
US5454627A (en) * 1993-07-27 1995-10-03 Bridgestone Corporation Method of correcting weight unbalance of rim-fitted tire
US5959204A (en) * 1993-10-26 1999-09-28 Hofmann Werkstatt-Technik Gmbh Method and apparatus for holding in position a motor vehicle wheel clamped on a balancing machine measuring spindle
US5889206A (en) * 1995-10-04 1999-03-30 Muller Bem Process and device for balancing a rotating body by addition of balancing weights
US5909097A (en) * 1996-09-06 1999-06-01 Hofmann Werkstatt-Technik Gmbh Method of stopping an electric motor-driven balancing machine main shaft
GB2323932A (en) * 1997-04-03 1998-10-07 Cirrus Technologies Ltd Wheel balancing apparatus using positive feedback to cause torsional instability
EP1321755A3 (en) * 2001-12-12 2005-05-25 Snap-On Equipment GmbH Method and device for balancing a vehicle wheel by rotating the wheel
EP1321755A2 (en) * 2001-12-12 2003-06-25 Snap-On Equipment GmbH Method and device for balancing a vehicle wheel by rotating the wheel
US20040070388A1 (en) * 2002-10-09 2004-04-15 Chuang Thomas Hong Detecting rotational direction of a rotating article
WO2004048917A2 (en) * 2002-11-26 2004-06-10 Bombardier Transportation Gmbh Rotating equipment testing apparatus and method
WO2004048917A3 (en) * 2002-11-26 2007-11-15 Bombardier Transp Gmbh Rotating equipment testing apparatus and method
US20040237647A1 (en) * 2003-06-02 2004-12-02 Youells James P. Drive location compensation system
US6829935B1 (en) * 2003-06-02 2004-12-14 Illinois Tool Works Inc. Drive location compensation system
US9146171B1 (en) * 2012-02-22 2015-09-29 Hennessy Industries, Inc. Auto calibration method and apparatus for wheel balancer equipment
US11333569B2 (en) * 2018-09-14 2022-05-17 Akron Special Machinery, Inc. Dynamic balancer with a frameless motor drive

Also Published As

Publication number Publication date
IT1085915B (en) 1985-05-28
JPS5296589A (en) 1977-08-13
DE2705023A1 (en) 1977-09-22
FR2340545B3 (en) 1979-10-05
NL7701065A (en) 1977-08-11
CA1101523A (en) 1981-05-19
FR2340545A1 (en) 1977-09-02
BE851064A (en) 1977-05-31

Similar Documents

Publication Publication Date Title
US4085619A (en) Electronic balancer for vehicle wheels
CA1070518A (en) Wheel balancing apparatus
JP3792718B2 (en) Angle measurement method for rotating body
US4785242A (en) Position detecting apparatus using multiple magnetic sensors for determining relative and absolute angular position
US4223386A (en) Method and apparatus for assembling tire with disc wheel
US4300197A (en) Process and apparatus for the centering of bodies of rotation having uneven mass distribution along their shaft axis
JPH0419496B2 (en)
US5329814A (en) Apparatus for turning a body to be balanced into a working position
CN106871850A (en) Angle measurement unit and the method for operation angle measurement apparatus
US4759217A (en) Process and apparatus for balancing a vehicle wheel
US3596100A (en) Linear output torque meter utilizing light sensing
US2730899A (en) Dynamic balancing apparatus
CN211085296U (en) Novel wheel-side encoder bracket
US4155255A (en) Read-out system for wheel balancer
US5488861A (en) Wheel balancer apparatus and method
US6563109B1 (en) Apparatus for optoelectronically determining power using a light source being of annular design
JPH087142Y2 (en) Bearing wear monitoring device
US3238785A (en) Wheel unbalance detection
JP2521563B2 (en) Method and device for inputting the parameters of a rotating body to the evaluation means of a balance tester
US5307279A (en) Self diagnostic wheel balancer
JPS59147231A (en) Flexible coupling for measuring torque
US3788147A (en) Device for the balancing of out of balance bodies especially vehicle wheels
SU976324A1 (en) Bearing radial clearence determination method
US3710627A (en) Gyroscopic-action dynamic balancer
WO1999011999A1 (en) Method and apparatus for measuring rotation motion

Legal Events

Date Code Title Description
AS Assignment

Owner name: BRANICK INDUSTRIES, INC., 2600 - 3RD AVE. NO., FAR

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:RUGBY INDUSTRIES, INC. A CORP. OF ND;REEL/FRAME:004938/0741

Effective date: 19870928